From fc397df94b086ea0e5e3c722feb90c4c7f5988c2 Mon Sep 17 00:00:00 2001 From: Anin Arafath <65447144+aninarafath6@users.noreply.github.com> Date: Sat, 15 Apr 2023 16:26:47 +0530 Subject: [PATCH 1/9] more clear readme data --- README.md | 22 +++++++++++++++------- 1 file changed, 15 insertions(+), 7 deletions(-) diff --git a/README.md b/README.md index f870093..b8090b6 100644 --- a/README.md +++ b/README.md @@ -1,10 +1,18 @@ -# ISRO 🚀 API +# ISRO Open Source API for Launched Spacecrafts & Rockets Data -Open Source API for Launched Spacecrafts & Rockets data of ISRO +Welcome to the ISRO Open Source API for Launched Spacecrafts & Rockets Data! This API provides access to data about ISRO spacecrafts, launchers, customer satellites, and centres. -## API End-Points +## Getting Started + +To get started with the API, you'll need to request an API key by emailing us at [insert email address here]. Once you receive your API key, you can start making requests to the API. + +## Endpoints + +The API provides the following endpoints: + +### Spacecrafts + +The `/api/spacecrafts` endpoint returns data about ISRO spacecrafts. The data includes the name of the spacecraft, the type of spacecraft, the launch date, and the mission details. + +Example Request: -- Spacecrafts: [/api/spacecrafts](https://isro.vercel.app/api/spacecrafts) -- Launchers: [/api/launchers](https://isro.vercel.app/api/launchers) -- Customer Satellites: [/api/customer_satellites](https://isro.vercel.app/api/customer_satellites) -- Centres: [/api/centres](https://isro.vercel.app/api/centres) From 4673cc3a9e8afd14ae237ea5165dc5b058a8ea16 Mon Sep 17 00:00:00 2001 From: Anin Arafath <65447144+aninarafath6@users.noreply.github.com> Date: Sat, 15 Apr 2023 16:29:34 +0530 Subject: [PATCH 2/9] Update README.md Edited docs details --- README.md | 4 ---- 1 file changed, 4 deletions(-) diff --git a/README.md b/README.md index b8090b6..2ace3c8 100644 --- a/README.md +++ b/README.md @@ -2,10 +2,6 @@ Welcome to the ISRO Open Source API for Launched Spacecrafts & Rockets Data! This API provides access to data about ISRO spacecrafts, launchers, customer satellites, and centres. -## Getting Started - -To get started with the API, you'll need to request an API key by emailing us at [insert email address here]. Once you receive your API key, you can start making requests to the API. - ## Endpoints The API provides the following endpoints: From 4111ef89c93135fedee480230f968ad107adb5d9 Mon Sep 17 00:00:00 2001 From: Anin Arafath Date: Sat, 15 Apr 2023 21:38:47 +0530 Subject: [PATCH 3/9] raw mission data json --- data/missions.json | 0 package-lock.json | 14 ++++++++++++++ 2 files changed, 14 insertions(+) create mode 100644 data/missions.json create mode 100644 package-lock.json diff --git a/data/missions.json b/data/missions.json new file mode 100644 index 0000000..e69de29 diff --git a/package-lock.json b/package-lock.json new file mode 100644 index 0000000..76fcc8d --- /dev/null +++ b/package-lock.json @@ -0,0 +1,14 @@ +{ + "name": "isro-api", + "version": "0.1.0", + "lockfileVersion": 3, + "requires": true, + "packages": { + "": { + "name": "isro-api", + "version": "0.1.0", + "license": "MIT", + "devDependencies": {} + } + } +} From f84b06144db005eec263b84ef2eb3f8579ca35e8 Mon Sep 17 00:00:00 2001 From: Anin Arafath Date: Sat, 15 Apr 2023 21:46:07 +0530 Subject: [PATCH 4/9] cleaned data about space craft missions --- data/missions.json | 968 +++++++++++++++++++++++++++++++++++++++++++++ 1 file changed, 968 insertions(+) diff --git a/data/missions.json b/data/missions.json index e69de29..72ae8e5 100644 --- a/data/missions.json +++ b/data/missions.json @@ -0,0 +1,968 @@ +[ +{ +"name": "RISAT-2BR1", +"id": 65, +"lift-off_weight": "628 kg", +"altitude": "576 km", +"payload": "X-Band Radar", +"inclination": "37 deg", +"mission_life": "5 years" +}, +{ +"name": "Cartosat-3", +"id": 64, +"mean________________________________________________________________altitude": "509 km", +"mean_inclination": "97.5\u00b0", +"overall_mass": "1625 kg", +"power_generation": "2000W", +"mission_life": "5 years" +}, +{ +"name": "GSAT-15", +"id": 63, +"mission": "Communication and Satellite Navigation", +"weight": "3164 kg (Mass at Lift \u2013 off) 1440 kg (Dry Mass)", +"power": "Solar array providing 6200 Watts and Three 100 AH Lithium-Ion batteries", +"propulsion": "Bi- propellant System", +"launch____________________________________________________________date": "November 11, 2015", +"launch____________________________________________________________site": "Kourou, French Guiana", +"launch____________________________________________________________vehicle": "Ariane-5 VA-227", +"orbit": "Geostationary (93.5\u00b0 East longitude)Co-located with INSAT-3A and INSAT-4B", +"mission____________________________________________________________life": "12 Years" +}, +{ +"name": "GSAT-6", +"id": 62, +"physical____________________________________________________________properties": "Lift off Mass : 2117 kg Main Structure : I-2K Overall size(m) : 2.1 x 2.5 x 4.1", +"power": "Generated power 3100 W", +"aocs": "Momentum biased 3-axis stabilised", +"antennas": "One 0.8 m (fixed) and one 6 m unfurlable antenna (transmit and receive)", +"communication____________________________________________________________payloads": "i. S-band payload with five spot beams covering India for user links ii. C-band payload with one beam covering India for hub links S-band payload uses 6 m unfurlable antenna and C-band uses 0.8 m antenna.", +"mission_life": "9 years" +}, +{ +"name": "IRNSS-1B", +"id": 61, +"off_mass": "1432 kg", +"physical_dimensions": "1.58 metre x 1.50 metre x 1.50 metre", +"orbit": "Geosynchronous, at 55 deg East longitude with 29 deg inclination", +"power": "Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity", +"propulsion": "440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters", +"control_system": "Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators", +"mission_life": "10 years", +"launch_date": "Apr 04, 2014", +"launch_site": "SDSC SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV - C24" +}, +{ +"name": "GSAT-14", +"id": 60, +"mass_at_lift-off": "1982 kg", +"overall_size_(m)": "2.0 X 2.0 X 3.6", +"power": "2600 W", +"attitude_and_orbit_control_system_(aocs)": "Momentum biased 3-axis stabilized mode", +"propulsion_system": "Bi propellant-Mono Methyl Hydrazine and Mixed Oxides of Nitrogen (MON-3)", +"antennae": "One 2m and one 2.2 m single shell shaped reflector Antennae (transmit and receive)", +"launch_date": "January 05, 2014", +"launch_site": "SDSC, SHAR", +"launch_vehicle": "GSLV-D5", +"orbit": "74 deg East longitude in geostationary orbit", +"mission_life": "12 Years" +}, +{ +"name": "GSAT-7", +"id": 59, +"mission": "Communication", +"mass_at_lift-off": "2650 kg", +"physical_dimensions": "3.1 m X 1.7 m X 2.0 m", +"power": "3,000 W (end of life)", +"satbilisation": "3-axis stabilized", +"launch_date": "August 30, 2013", +"launch_site": "Kourou, French Guiana", +"launch_vehicle": "Ariane-5 VA-215", +"orbit": "74oE Geo Stationary", +"mission_life": "> 7 Years" +}, +{ +"name": "INSAT-3D", +"id": 58, +"mission": "Meteorological and Search & Rescue Services", +"mass_at_lift-off": "2060 kg", +"power": "Solar panel generating 1164 W Two 18 Ah Ni-Cd batteries", +"physical_dimensions": "2.4m x 1.6m x 1.5m", +"propulsion": "440 Newton Liquid Apogee Motor (LAM) and twelve 22 Newton thrusters with Mono Methyl Hydrazine (MMH) as fuel and mixed Oxides of Nitrogen (MON-3) as oxidizer", +"stabilisation": "3-asix body stabilized in orbit using Sun Sensors, Star Sensors, gyroscopes, Momentum and Reaction Wheels, Magnetic Torquers and thrusters", +"antennae": "0.9m and 1.0m body mounted antennas", +"launch_date": "July 26, 2013", +"launch_site": "Kourou, French Guiana", +"launch_vehicle": "Ariane-5 VA-214", +"orbit": "Geostationary, 82 deg E Longitude", +"mission_life": "7 Years" +}, +{ +"name": "IRNSS-1A", +"id": 57, +"lift-off_mass": "1425 kg", +"physical_dimensions": "1.58 metre x 1.50 metre x 1.50 metre", +"orbit": "Geosynchronous, at 55 deg East longitude with 29 deg inclination", +"power": "Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity", +"propulsion": "440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters", +"control_system": "Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators", +"mission_life": "10 years", +"launch_date": "Jul 01, 2013", +"launch_site": "SDSC SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV - C22" +}, +{ +"name": "SARAL", +"id": 56, +"lift-off_mass": "407 kg", +"orbit": "781 km polar Sun synchronous", +"sensors": "4 PI sun sensors, magnetometer, star sensors and miniaturised gyro based Inertial Reference Unit", +"orbit_inclination": "98.538o", +"local_time_of_equator": "18:00 hours crossing", +"power": "Solar Array generating 906 W and 46.8 Ampere-hour Lithium-ion battery", +"onboard_data_storage": "32 Gb", +"attitude_and_orbit_control": "3-axis stabilisation with reaction wheels, Hydrazine Control System based thrusters", +"mission_life": "5 years", +"launch_date": "Feb 25, 2013", +"launch_site": "SDSC SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV - C20" +}, +{ +"name": "GSAT-10", +"id": 55, +"mission": "Communication", +"weight": "3400 kg (Mass at Lift \u2013 off) 1498 kg (Dry Mass)", +"power": "Solar array providing 6474 Watts (at Equinox) and two 128 AH Lithium-Ion batteries", +"physical_dimensions": "2.0 m X 1.77 m X 3.1 m cuboid", +"propulsion": "440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", +"stabilisation": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", +"antennae": "East : 2.2 m dia circular deployable Dual Gridded Reflector (DGR) West : 2.2 m X 2.4 m elliptical deployable DGR Earth Viewing Face (top) : 0.7 m parabolic, 0.9 m parabolic and 0.8 m X 0.8 m sixteen element helical antenna for GAGAN", +"launch_date": "September 29, 2012", +"launch_site": "Kourou, French Guiana", +"launch_vehicle": "Ariane-5 VA-209", +"orbit": "Geostationary (83\u00b0 East longitude), co-located with INSAT-4A and GSAT-12", +"mission_life": "15 Years" +}, +{ +"name": "RISAT-1", +"id": 54, +"mass": "1858 kg", +"orbit": "Circular Polar Sun Synchronous", +"orbit_altitude": "536 km", +"orbit_inclination": "97.552o", +"orbit_period": "95.49 min", +"number_of_orbits_per_day": "14", +"local_time_of_equator_crossing": "6:00 am / 6:00 pm", +"power": "Solar Array generating 2200 W and one 70 AH Ni-H2 battery", +"repetivity": "25 days", +"attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", +"nominal_mission_life": "5 years", +"launch_date": "April 26, 2012", +"launch_site": "SDSC SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV- C19" +}, +{ +"name": "Megha-Tropiques", +"id": 53, +"lift-off_mass": "1000 kg", +"orbit": "867 km with an inclination of 20 deg to the equator", +"thermal": "Passive system with IRS heritage", +"power": "1325 W (at End of Life) Two 24 AH NiCd batteries", +"ttc": "S-band", +"attitude_and_orbit_control": "3-axis stabilised with 4 Reaction Wheels, Gyros and Star sensors, Hydrazine based RCS", +"solid_state_recorder": "16 Gb", +"launch_date": "October 12, 2011", +"launch_site": "SDSC SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV- C18" +}, +{ +"name": "GSAT-12", +"id": 52, +"mission": "Communication", +"weight": "1410 kg (Mass at Lift \u2013 off) 559 kg (Dry Mass)", +"power": "Solar array providing 1430 Watts and one 64 Ah Li-Ion batteries", +"physical_dimensions": "1.485 x 1.480 x 1.446 m cuboid", +"propulsion": "440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", +"attitude_orbit_control": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", +"antennae": "One 0.7 m diameter body mounted parabolic receive antenna and one 1.2 m diameter polarisation sensitive deployable antenna", +"launch_date": "July 15, 2011", +"launch_site": "SHAR, Sriharikota, India", +"launch_vehicle": "PSLV-C17", +"orbit": "Geosynchronous (83\u00b0 longitude)", +"mission_life": "About 8 Years" +}, +{ +"name": "GSAT-8", +"id": 51, +"mission": "Communication", +"weight": "3093 kg (Mass at Lift \u2013 off) 1426 kg (Dry Mass)", +"power": "Solar array providing 6242 watts three 100 Ah Lithium Ion batteries", +"physical_dimensions": "2.0 x 1.77 x 3.1m cuboid", +"propulsion": "440 Newton Liquid Apogee Motors (LAM) with mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", +"stabilisation": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", +"antennas": "Two indigenously developed 2.2 m diameter transmit/receive polarisation sensitive dual grid shaped beam deployable reflectors with offset-fed feeds illumination for Ku-band; 0.6 m C-band and 0.8x0.8 sq m L-band helix antenna for GAGAN", +"launch_date": "May 21, 2011", +"launch_site": "Kourou, French Guiana", +"launch_vehicle": "Ariane-5 VA-202", +"orbit": "Geosynchronous (55\u00b0 E)", +"mission_life": "More Than 12 Years" +}, +{ +"name": "RESOURCESAT-2", +"id": 50, +"mission": "Remote Sensing", +"orbit": "Circular Polar Sun Synchronous", +"orbit_altitude_at_injection": "822 km + 20 km (3 Sigma)", +"orbit_inclination": "98.731\u00ba + 0.2\u00ba", +"lift-off_mass": "1206 kg", +"orbit_period": "101.35 min", +"number_of_orbits_per_day": "14", +"local_time_of_equator_crossing": "10:30 am", +"repetivity": "24 days", +"attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", +"power": "Solar Array generating 1250 W at End Of Life, two 24 AH Ni-Cd batteries", +"launch_date": "April 20, 2011", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C16", +"mission_life": "5 years" +}, +{ +"name": "YOUTHSAT", +"id": 49, +"lift-off_mass": "92 kg", +"orbit_period": "101.35 min", +"dimension": "1020 (Pitch) x 604 (Roll) x 1340 (Yaw) mm3", +"attitude_and_orbit_control": "3-axis body stabilised using Sun and Star Sensors, Miniature Magnetometer, Miniature Gyros, Micro Reaction Wheels and Magnetic Torquers", +"power": "Solar Array generating 230 W, one 10.5 AH Li-ion battery", +"mechanisms": "Paraffin Actuator based Solar Panel Hold Down and Release Mechanism", +"launch_date": "April 20, 2011", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C16", +"orbit": "Circular Polar Sun Synchronous", +"orbit_altitude_at_injection": "822 km\u00a0+\u00a020 km (3 Sigma)", +"orbit_inclination": "98.731 \u00ba\u00a0+\u00a00.2 \u00ba", +"mission_life": "2 years" +}, +{ +"name": "CARTOSAT-2B", +"id": 48, +"mission": "Remote Sensing", +"weight": "694 kg (Mass at lift off)", +"onboard_orbit": "930 Watts", +"stabilization": "3 \u2013 axis body stabilised based on inputs from star sensors and gyros using Reaction wheels, Magnetic Torquers and Hydrazine Thrusters", +"payloads": "Panchromatic Camera", +"launch_date": "July 12, 2010", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C15", +"orbit": "630 kms, Polar Sun Synchronous", +"inclination": "97.71\u00ba" +}, +{ +"name": "Oceansat-2", +"id": 47, +"date": "Sept 23, 2009", +"launch_site": "SHAR, Sriharikota", +"launch_vehicle": "PSLV - C14", +"orbit": "Polar Sun Synchronous", +"altitude": "720 km", +"inclination": "98.28\u00b0", +"period": "99.31 minutes", +"local_time_of_eq._crossing": "12 noon \u00b1 10 minutes", +"repetitivity_cycle": "2 days", +"payloads": "OCM, SCAT and ROSA", +"mass_at_lift_off": "960 kg", +"power": "15 Sq.m Solar panels generating 1360W, Two 24 Ah Ni-Cd Batteries", +"mission_life": "5 years" +}, +{ +"name": "RISAT-2", +"id": 46, +"altitude": "550 km", +"inclination": "41 deg", +"orbit_period": "90 minutes", +"mass": "300 kg" +}, +{ +"name": "Chandrayaan-1 ", +"id": 45, +"mission": "Remote Sensing, Planetary Science", +"weight": "1380 kg (Mass at lift off)", +"onboard_power": "700 Watts", +"stabilization": "3 - axis stabilised using reaction wheel and attitude control thrusters, sun sensors, star sensors, fibre optic gyros and accelerometers for attitude determination.", +"launch_date": "22 October 2008", +"launch_site": "SDSC, SHAR, Sriharikota", +"launch_vehicle": "PSLV - C11", +"orbit": "100 km x 100 km : Lunar Orbit", +"mission_life": "2 years" +}, +{ +"name": "IMS-1", +"id": 44, +"orbit": "Polar Sun Synchronous", +"altitude": "635 km", +"mission_life": "2 years", +"physical_dimensions": "0.604x0.980x1.129 m", +"mass": "83 kg", +"power": "Two deployable sun pointing solar panels generating 220 W power, 105 Ah Lithium ion battery", +"telemetry,_tracking_and_command": "S-band", +"attitude_and_orbit_control_system": "Star Sensor, Miniature Sun Sensors, Magnetometers Gyros, Miniature Micro Reaction Wheels, Magnetic Torquers, single 1 N Hydrazine Thruster", +"data_handling": "S-band", +"data_storage": "16 Gb Solid State Recorder" +}, +{ +"name": "CARTOSAT \u2013\n2A", +"id": 43, +"mission": "Remote Sensing", +"weight": "690 Kg (Mass at lift off)", +"onboard_power": "900 Watts", +"stabilization": "3 \u2013 axis body stabilised using high torque reaction wheels, magnetic torquers and hydrogen thrusters", +"payloads": "Panchromatic Camera", +"launch_date": "28 April 2008", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C9", +"orbit": "635 km, Polar Sun Synchronous", +"inclination": "97.94 deg", +"mission_life": "5 years" +}, +{ +"name": "INSAT-4CR", +"id": 42, +"mission": "Communication", +"weight": "2,130 kg (Mass at Lift \u2013 off)", +"onboard_power": "3000 W", +"communication_payload": "12 Ku-band transponders employing 140 W Traveling Wave Tube Amplifiers (TWTA) Ku-band Beacon", +"launch_date": "September 2, 2007", +"launch_site": "SHAR, Sriharikota, India", +"launch_vehicle": "GSLV-F04", +"orbit": "Geosynchronous (74\u00b0 E)", +"mission_life": "12 Years" +}, +{ +"name": "INSAT-4B", +"id": 41, +"mission": "Communication", +"weight": "3025 kg (at Lift \u2013 off)", +"onboard_power": "5859 W", +"stabilization": "It uses 3 earth sensors, 2 digital sun sensors, 8 coarse analog sun sensors, 3 solar panel sun sensors and one sensor processing electronics. The wheels and wheel drive electronics were imported with indigenous wheel interface module to interface the wheel drive electronics and AOCE.", +"propulsion": "The propulsion system is employing 16 thrusters, 4 each located on east, west and AY sides and 2 each on north and south sides. There is one 440 N liquid apogee motor (using Mono Methyl Hydrazine (MMH) as fuel and oxides of Nitrogen (MON3 as oxidizer) and three pressurant tanks mounted on the LAM deck.", +"payload": "12 Ku band high power transponders covering Indian main land using 140W radiatively cooled TWTAs.", +"launch_date": "March 12, 2007", +"launch_site": "French Guiana", +"launch_vehicle": "Ariane5", +"orbit": "Geostationary (93.5o E Longitude)", +"mission_life": "12 Years" +}, +{ +"name": "CARTOSAT-2", +"id": 40, +"mission": "Remote Sensing", +"weight": "650 Kg", +"onboard_orbit": "900 Watts", +"stabilization": "3 - axis body stabilised using high torque reaction wheels, magnetic torquers and thrusters", +"payloads": "Panchromatic Camera", +"launch_date": "10 January 2007", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C7", +"orbit": "Polar Sun Synchronous", +"mission_life": "5 years" +}, +{ +"name": "INSAT-4A", +"id": 39, +"spacecraft_mass": "Lift off 3081 Kg Dry Mass 1386.55 Kg", +"orbit": "Geostationary ( 83o E)", +"power": "Solar Array to provide a power of 5922 W", +"battery": "Three 70 Ah Ni H2 Batteries for eclipse support of 4264 W", +"life": "12 Years", +"launch_date": "December 22, 2005", +"launch_vehicle": "ARIANE5-V169" +}, +{ +"name": "CARTOSAT-1", +"id": 38, +"launch_date": "5 May 2005", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C6", +"orbit": "618 km Polar Sun Synchronous", +"payloads": "PAN FORE, PAN - AFT", +"orbit_period": "97 min", +"number_of_orbits_per_day": "14", +"local_time_of_equator_crossing": "10:30 am", +"repetivity": "126 days", +"revisit": "5 days", +"lift-off_mass": "1560 kg", +"attitude_and_orbit_control": "3-axis body stabillised using reaction wheels, Magnetic Torquers and Hydrazine Thrusters", +"electrical_power": "15 sqm Solar Array generating 1100w, Two 24 Ah Ni-Cd batteries", +"mission_life": "5 years" +}, +{ +"name": "HAMSAT", +"id": 37, +"launch_date": "May 5, 2005", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV-C6", +"orbit": "Geo-synchronous, 633.355 km (average)", +"payloads": "2 Transponders" +}, +{ +"name": "EDUSAT", +"id": 36, +"mission": "Education", +"spacecraft_mass": "1950.5 kg mass (at Lift - off) 819.4 kg (Dry mass)", +"onboard_power": "Total four solar panel of size 2.54 M x 1.525 M generating 2040 W (EOL), two 24 AH NiCd batteries for eclipse support", +"stabilization": "3 axis body stabilised in orbit using sensors, momentum and reaction wheels, magnetic torquers and eight 10 N & 22N reaction control thrusters.", +"propulsion": "440 N Liquid Apogee Motor with MON - 3 and MMH for orbit raising", +"payload": "Six upper extended C - band transpondersFive lower Ku band transponders with regional beam coverage One lower Ku band National beam transponder with Indian main land coverageKu beacon12 C band high power transponders with extended coverage, covering southeast and northwest region apart from Indian main land using 63 W LTWTAs", +"launch_date": "September 20, 2004", +"launch_site": "SHAR, Sriharikota, India", +"launch_vehicle": "GSLV-F01", +"orbit": "Geostationary (74oE longitude)", +"mission_life": "7 Years (minimum)" +}, +{ +"name": "IRS-P6 / RESOURCESAT-1", +"id": 35, +"launch_date": "October 17, 2003", +"launch_site": "SHAR, Sriharikota", +"launch_vehicle": "PSLV-C5", +"payloads": "LISS-4, LISS-3, AWiFS-A, AWiFS-B", +"orbit": "Polar Sun Synchronous", +"orbit_height": "817 km", +"orbit_inclination": "98.7o", +"orbit_period": "101.35 min", +"number_of_orbits_per_day": "14", +"local_time_of_equator_crossing": "10:30 am", +"repetivity_(liss-3)": "24 days", +"revisit": "5 days", +"lift-off_mass": "1360 kg", +"attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", +"power": "Solar Array generating 1250 W, Two 24 Ah Ni-Cd batteries", +"mission_life": "5 years" +}, +{ +"name": "INSAT-3E", +"id": 34, +"mission": "Communication", +"spacecraft_mass": "2,775 kg (Mass at Lift-off) 1218 kg (Dry mass)", +"launch_date": "September 28, 2003", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane5-V162", +"orbit": "Geostationary Orbit" +}, +{ +"name": "GSAT-2", +"id": 33, +"mission": "Communication", +"weight": "1800 kg", +"launch_date": "May 8, 2003", +"launch_site": "SHAR, Sriharikota, India", +"launch_vehicle": "GSLV\u2013D2", +"orbit": "Geostationary orbit (48oE longitude)" +}, +{ +"name": "INSAT-3A", +"id": 32, +"mission": "Telecommunication, broadcasting and Meteorology", +"spacecraft_mass": "2,950 kg (Mass at Lift\u2013off) 1,348 kg (Dry mass)", +"onboard_power": "3,100 W", +"stabilization": "3 \u2013 axis body stabilised in orbit using momentum and reaction wheels, solar flaps, magnetic torquers and eight 10 N and eight 22 N reaction control thrusters", +"propulsion": "440 N Liquid Apogee Motor with MON-3 (Mixed Oxides of Nitrogen) and MMH (Mono Methyl Hydrazine) for orbit raising", +"payload": "Communication payload- 12 C \u2013 band transponders, - 6 upper extended C band transponders - 6 Ku band transponders - 1 Satellite Aided Search & Rescue transponders Meteorological payload- Very High Resolution Radiometer (VHRR) with 2 km resolution in visible band and 8 km resolution in infrared and water vapour band- Charged Coupled Device (CCD) camera operating in visible, near infrared and shortwave infrared band with 1 km resolution.- Data Relay Transponders (DRT)", +"launch_date": "April 10, 2003", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane5-V160", +"orbit": "Geostationary (93.5o E longitude)", +"mission_life": "12 Years" +}, +{ +"name": "KALPANA-1", +"id": 31, +"mission": "7 Years", +"spacecraft_mass": "1060 kg mass (at Lift \u2013 off) 498 kg (Dry mass)", +"onboard_power": "550 W", +"payload": "Very High Resolution Radiometer (VHRR) Data Relay Transponder (DRT)", +"launch_date": "12 September 2002", +"launch_site": "SHAR, Sriharikota", +"launch_vehicle": "PSLV \u2013 C4", +"orbit": "Geostationary (74 deg East longitude)" +}, +{ +"name": "INSAT-3C", +"id": 30, +"mission": "Communication, broadcasting and Meteorology", +"spacecraft_mass": "2,650 kg (Mass at Lift - off) 1218 kg (Dry mass)", +"onboard_power": "2765 W", +"propulsion": "Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.", +"payload": "24 C band transponders 6 Extended C - band Transponders 2 S - band Transponders", +"launch_date": "January 24, 2002", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane5-V147", +"orbit": "Geostationary (74o longitude)", +"mission_life": "Very long" +}, +{ +"name": "The Technology Experiment Satellite\n(TES)", +"id": 29, +"launch_date": "22 October 2001", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C3", +"orbit": "572 km Sun Synchronous", +"payloads": "PAN" +}, +{ +"name": "PSLV-C3 / TES", +"id": 28, +"launch_date": "22 October 2001", +"launch_site": "SHAR Centre Sriharikota India", +"launch_vehicle": "PSLV- C3", +"orbit": "572 km Sun Synchronous", +"payloads": "PAN" +}, +{ +"name": "GSAT-1", +"id": 27, +"mission": "Communication", +"weight": "1530 kg", +"launch_date": "18 April 2001", +"launch_site": "SHAR, Sriharikota", +"launch_vehicle": "GSLV \u2013 D1", +"orbit": "Sun Synchronous Geo stationary orbit" +}, +{ +"name": "INSAT-3B", +"id": 26, +"mission": "Very long", +"spacecraft_mass": "2,070 (Mass at Lift \u2013 off) 970 kg (Dry mass)", +"onboard_power": "1,712 W", +"stabilization": "3 \u2013 axis body stabilised biased momentum control system using earth sensors, sun sensors, inertial reference unit, momentum / reaction wheels, magnetic torquers and unified bi-propellant thrusters.", +"propulsion": "Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.", +"payload": "12 extended C \u2013 band Transponders Five Ku band Transponders Mobile Satellite Services (MSS)", +"launch_date": "22nd March 2000", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane -5", +"orbit": "Geostationary (83 deg East longitude)", +"inclination": "7 deg" +}, +{ +"name": "Oceansat(IRS-P4)", +"id": 25, +"launch_date": "May 26, 1999", +"launch_site": "SHAR, Sriharikota", +"launch_vehicle": "PSLV - C2", +"orbit": "Polar Sun Synchronous", +"altitude": "720 km", +"inclination": "98.28 deg", +"period": "99.31 min", +"local_time_of_eq._crossing": "12 noon", +"repetitivity_cycle": "2 days", +"size": "2.8m x 1.98m x 2.57m", +"mass_at_lift_off": "1050 kg", +"length_when_fully_deployed": "11.67 m", +"attitude_and_orbit_control": "3-axis body-stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", +"power": "9.6 Sq.m Solar Array generating 750w Two 21 Ah Ni-Cd Batteries", +"mission_completed_on": "August 8, 2010" +}, +{ +"name": "INSAT-2E", +"id": 24, +"mission": "Communication and Meteorology", +"spacecraft_mass": "2,550 kg (Mass at Lift-off) 1150 kg (Dry mass)", +"launch_date": "03 April 1999", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane \u2013 42P", +"orbit": "Geosynchronous (83 deg east longitude)" +}, +{ +"name": "IRS-1D", +"id": 23, +"mission": "Operational Remote Sensing", +"weight": "1250 kg", +"onboard_power": "809 Watts (generated by 9.6 sq.metres Solar Panels)", +"communication": "S-band, X-band", +"stabilization": "Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer", +"rcs": "Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters", +"payload": "Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)", +"onboard_tape_recorder": "Storage Capacity : 62 G bits", +"launch_date": "December 28, 1995", +"launch_site": "Baikanur Cosmodrome Kazakhstan", +"launch_vehicle": "Molniya", +"orbit": "817 km Polar Sun-synchronous", +"inclination": "98.69o", +"repetivity": "24 days", +"local_time": "10.30 a.m", +"mission_completed_on": "September 21, 2007" +}, +{ +"name": "INSAT-2D", +"id": 22, +"mission": "Communication", +"weight": "2079 kg with propellants, 995 kg dry weight", +"onboard_power": "1650 Watts", +"communication": "C, extended C, S and Ku bands", +"stabilization": "Three axis stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", +"propulsion": "Integrated bipropellan stystem ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.", +"payload": "Transponders: 16C-band / extended C-band transponders (forFSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders", +"launch_date": "June 4, 1997", +"launch_site": "French Guyana", +"launch_vehicle": "Arianev 4", +"orbit": "Geostationary 93,.5deg.E", +"inclination": "0 deg." +}, +{ +"name": "IRS-P3", +"id": 21, +"mission": "Remote sensing of earth's natural resources. Study of X-ray Astronomy. Periodic calibration of PSLV tracking radar located at tracking stations.", +"weight": "920 kg", +"onboard_power": "817 Watts", +"communication": "S-band", +"stabilization": "Three axis body stabilized", +"rcs": "Combinations of bladder type and surface tension type mass expulsion monopropellant hydrazine system", +"payload": "WideField Sensor (WiFS), Modular Opto - electronic Scanner (MOS), Indian X-ray Astronomy Experiment (IXAE), C-band transponder(CBT)", +"launch_date": "March 21, 1996", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV-D3", +"orbit": "817 km. Circular polar sun-synchronous with equatorial crossing at 10.30 am (descending node)", +"inclination": "98.68o", +"repetivity": "WiFS : 5 days", +"mission_completed_during": "January 2006" +}, +{ +"name": "IRS-1C", +"id": 20, +"mission": "Operational Remote Sensing", +"weight": "1250 kg", +"onboard_power": "809 Watts (generated by 9.6 sq.metres Solar Panels)", +"communication": "S-band, X-band", +"stabilization": "Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer", +"rcs": "Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters", +"payload": "Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)", +"onboard_tape_recorder": "Storage Capacity : 62 G bits", +"launch_date": "December 28, 1995", +"launch_site": "Baikanur Cosmodrome Kazakhstan", +"launch_vehicle": "Molniya", +"orbit": "817 km Polar Sun-synchronous", +"inclination": "98.69o", +"repetivity": "24 days", +"local_time": "10.30 a.m", +"mission_completed_on": "September 21, 2007" +}, +{ +"name": "INSAT-2C", +"id": 19, +"mission": "Communication", +"weight": "2106 kg with propellants 946 kg dry weight", +"onboard_power": "1320 Watts", +"communication": "C extended C, S and Ku bands", +"stabilization": "Three axis stabilized with two Momen'tum Wheels & one Reaction Wheel, Magnetic torquers", +"propulsion": "Integrated bipropellant system ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.", +"payload": "Transponders: 16C-band / extended C-band transponders (for FSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders", +"launch_date": "December 7, 1995", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane4", +"orbit": "Geostationary 93.5 deg E", +"inclination": "0 deg.", +"mission_life": "Seven years(nominal)", +"orbit_life": "Very Long" +}, +{ +"name": "IRS-P2", +"id": 18, +"mission": "Operational Remote Sensing", +"weight": "804 kg", +"onboard_power": "510 Watts", +"communication": "S-band, X-band", +"stabilization": "Three axis body stabilized with 4 Reaction Wheels, Magnetic torquers", +"rcs": "4 tanks containing Monopropellant Hydrazine based with sixteen 1 N thrusters and one 11 N thruster", +"payload": "Two solid state Push Broom Cameras operating in four spectral bands in the visible and near-IR range using CCD arrays: LlSS-2A & LlSS-2B (Resolution: 32.74 metre)", +"launch_date": "October 15, 1994", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV-D2", +"inclination": "98.68o", +"repetivity": "24 days", +"mission_completed_on": "1997" +}, +{ +"name": "SROSS-C2", +"id": 17, +"mission": "Experimental", +"weight": "115 kg", +"onboard_power": "45 Watts", +"communication": "S-band and VHF", +"rcs": "Monopropellant Hydrazine based with six 1 Newton thrusters", +"payload": "Gamma Ray Burst (GRB) & Retarding Potential Analyser (RPA)", +"launch_date": "May 04,1994", +"launch_site": "SHAR Centre,Sriharikota,India", +"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", +"orbit": "430 x 600 km.", +"inclination": "45 deg.", +"mission_life": "Six months (nominal)", +"orbital_life": "Two years (nominal)" +}, +{ +"name": "IRS-1E", +"id": 16, +"mission": "Operational Remote Sensing", +"weight": "846 kg", +"onboard_power": "415 Watts", +"communication": "S-band (TIC) & VHF", +"stabilization": "Three axis body stabilized ( zero momentum) with 4 Reaction Wheels, Magnetic torquers", +"rcs": "Monopropellant Hydrazine based RCS with 1 Newton thrusters ( 16 Nos.)", +"payload": "LlSS-1 MEOSS (Mono-ocula Erlectro Optic Stereo Scanner)", +"launch_date": "September 20, 1993", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "PSLV-D1", +"orbit": "Not realised" +}, +{ +"name": "INSAT-2B", +"id": 15, +"mission": "Multipurpose Communication, meteorology and Satellite based search and rescue", +"weight": "1906 kg with propellant 916 kg dry weight", +"onboard_power": "One KW approx.", +"communication": "C, extended C and S band", +"stabilization": "Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", +"propulsion": "Integrated bipropellant system ( MMH and N2 04) With sixteen 22 N thrusters and 440 N LAM.", +"payload": "Transponders: 12C-band (for FSS),6 ext. C-band (for FSS) 2S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band", +"launch_date": "July 23, 1993", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane 4", +"orbit": "Geostationary 93.5o E", +"inclination": "0o", +"mission_life": "Seven years(nominal)", +"orbit_life": "Very Long" +}, +{ +"name": "INSAT-2A", +"id": 14, +"mission": "Multipurpose Communication, meteorology and Satellite based search and rescue", +"weight": "1906 kg with propellant 916 kg dry weight", +"onboard_power": "One KW approx", +"communication": "C, extended C and S band", +"stabilization": "Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", +"propulsion": "Integrated bipropellant system (MMH and N2 04) With sixteen 22 N thrusters and 440 LAM.", +"payload": "Transponders: 12 C-band (for FSS),6 ext. C-band (for FSS) 2 S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band", +"launch_date": "July 10,1992", +"launch_site": "French Guyana", +"launch_vehicle": "Ariane 4", +"orbit": "Geostationary 74oE longitude", +"inclination": "0o", +"mission_life": "Seven years(nominal)", +"orbit_life": "Very Long" +}, +{ +"name": "SROSS-C\n", +"id": 13, +"mission": "Experimental", +"weight": "106.1 kg", +"onboard_power": "45 Watts", +"communication": "S-band and VHF", +"stabilization": "Spin stabilized with a Magnetic Torquer and Magnetic Bias Control", +"payload": "Gamma Ray Burst (GRB) experiment & Retarding Potential Analyser (RPA) experiment", +"launch_date": "May 20,1992", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", +"orbit": "267 x 391 km", +"mission_life": "Two months (Re-entered on July15,1992)" +}, +{ +"name": "IRS-1B", +"id": 12, +"mission": "Operational Remote Sensing", +"weight": "975 kg", +"onboard_power": "600 Watts", +"communication": "S-band, X-band and VHF (commanding only)", +"stabilization": "Three axis body stabilized (zero momentum) with 4 Reactions Wheels, Magnetic torquers", +"rcs": "Monopropellant Hydrazine based with sixteen 1 Newton thrusters", +"payload": "Three solid state Push Broom Cameras LlSS-1 (72.5 metre resolution), LlSS-2A and LlSS-2B (36.25 metre resolution)", +"launch_date": "August 29, 1991", +"launch_site": "Baikanur Cosmodrome Kazakhstan", +"launch_vehicle": "Vostok", +"orbit": "904 km Polar Sun Synchronous", +"inclination": "99.08o", +"repetivity": "22 days", +"local_time": "10.30 a.m. (descending node)", +"mission_completed_on": "December 20, 2003" +}, +{ +"name": "SROSS-2", +"id": 11, +"mission": "Experimental", +"weight": "150 kg", +"onboard_power": "90 Watts", +"communication": "S-band and VHF", +"stabilization": "Three axis body stabilized (biased momentum) with a MomentumWheel and Magnetic Torquer", +"propulsion_system": "Monopropellant (Hydrazine based) Reaction Control System", +"payload": "Gamma Ray Burst (GRB) payload and Mono PayloadOcular Electro-Optic Stereo Scanner (MEOSS) built by DLR, Germany", +"launch_date": "July 13, 1988", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", +"orbit": "Not realised" +}, +{ +"name": "IRS-1A", +"id": 10, +"mission": "Operational Remote Sensing", +"weight": "975 kg", +"onboard_power": "600 Watts", +"communication": "S-band, X-band and VHF(commanding only)", +"stabilization": "Three axis body stabilized (zero momentum)with 4 Reactions Wheels, Magnetic torquers", +"rcs": "Monopropellant Hydrazine based with sixteen 1 Newton thrusters", +"payload": "Three solid state Push Broom Cameras: LISS-1(72.5 metre resolution),LISS-2A and LISS-2B (36.25 metre resolution)", +"launch_date": "March 17, 1988", +"launch_site": "Baikanur Cosmodrome Kazakhstan", +"launch_vehicle": "Vostok", +"orbit": "904 km Polar Sun-synchronous", +"inclination": "99.08o", +"repetivity": "22 days (307 orbits)", +"local_time": "10.30 a.m. (descending node)", +"mission_completed_during": "July 1996" +}, +{ +"name": "SROSS-1\n", +"id": 9, +"mission": "Experimental", +"weight": "150 kg", +"onboard_power": "90 Watts", +"communication": "S-band and VHF", +"stabilization": "Three axis body stabilized (biased momentum) with a Momentum Wheel and Magnetic Torquer", +"propulsion_system": "Monopropellant (Hydrazine based) Reaction control system", +"payload": "Launch Vehicle Monitoring Platform(LVMP), Gamma Ray Burst (GRB) payload and Corner Cube Retro Reflector (CCRR) for laser tracking", +"launch_date": "March 24, 1987", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", +"orbital_life": "Not realised" +}, +{ +"name": "Rohini Satellite RS-D2", +"id": 8, +"mission": "Experimental", +"weight": "41.5 kg", +"onboard_power": "16 Watts", +"communication": "VHF band", +"stabilization": "Spin stabilized", +"payload": "Smart sensor (remote sensing payload),L-band beacon", +"launch_date": "April 17, 1983", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "SLV-3", +"orbit": "371 x 861 km", +"inclination": "46o", +"mission_life": "17 months", +"orbital_life": "Seven years (Re-entered on April 19, 1990)" +}, +{ +"name": "Bhaskara-II", +"id": 7, +"mission": "Experimental Remote Sensing", +"weight": "444 kg", +"onboard_power": "47 Watts", +"communication": "VHF band", +"stabilization": "Spin stabilized (spin axis controlled)", +"payload": "TV cameras, three band Microwave Radiometer (SAMIR)", +"launch_date": "Nov 20, 1981", +"launch_site": "Volgograd Launch Station (presently in Russia)", +"launch_vehicle": "C-1 Intercosmos", +"orbit": "541 x 557 km", +"inclination": "50.7o", +"mission_life": "One year (nominal)", +"orbital_life": "About 10 years ( Re-entered in 1991 )" +}, +{ +"name": "APPLE", +"id": 6, +"mission": "Experimental geostationary communication", +"weight": "670 kg", +"onboard_power": "210 Watts", +"communication": "VHF and C-band", +"stabilization": "Three axis stabilized (biased momentum) with Momentum Wheels, Torquers & Hydrazine based Reaction control system", +"payload": "C - band transponders (Two)", +"launch_date": "June19,1981", +"launch_site": "Kourou (CSG), French Guyana", +"launch_vehicle": "Ariane -1(V-3)", +"orbit": "Geosynchronous (102 deg. E longitude, over Indonesia)", +"inclination": "Near zero", +"mission_life": "Two years" +}, +{ +"name": "Rohini Satellite RS-D1", +"id": 5, +"mission": "Experimental", +"weight": "38 kg", +"onboard_power": "16 Watts", +"communication": "VHF band", +"stabilization": "Spin stabilized", +"payload": "Landmark Tracker ( remote sensing payload)", +"launch_date": "May 31,1981", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "SLV-3", +"orbit": "186 x 418 km (achieved)", +"inclination": "46 deg", +"orbital_life": "Nine days" +}, +{ +"name": "Rohini Satellite RS-1", +"id": 4, +"mission": "Experimental", +"weight": "35 kg", +"onboard_power": "16 Watts", +"communication": "VHF band", +"stabilization": "Spin stabilized", +"payload": "Launch vehicle monitoring instruments", +"launch_date": "July 18,1980", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "SLV-3", +"orbit": "305 x 919 km", +"inclination": "44.7 deg.", +"mission_life": "1.2 years", +"orbital_life": "20 months" +}, +{ +"name": "Rohini Technology Payload (RTP)", +"id": 3, +"mission": "Experimental", +"weight": "35 kg", +"onboard_power": "3 Watts", +"communication": "VHF band", +"stabilization": "Spin stabilized (spin axis controlled)", +"payload": "Launch vehicle monitoring instruments", +"launch_date": "August 10,1979", +"launch_site": "SHAR Centre, Sriharikota, India", +"launch_vehicle": "SLV-3", +"orbit": "Not achieved" +}, +{ +"name": "Bhaskara-I", +"id": 2, +"mission": "Experimental Remote Sensing", +"weight": "442 kg", +"onboard_power": "47 Watts", +"communication": "VHF band", +"stabilization": "Spin stabilized (spin axis controlled)", +"payload": "TVcameras, three band Microwave Radiometer (SAMIR)", +"launch_date": "Jun 07,1979", +"launch_site": "Volgograd Launch Station (presently in Russia)", +"launch_vehicle": "C-1Intercosmos", +"orbit": "519 x 541 km", +"inclination": "50.6 deg", +"mission_life": "One year (nominal)", +"orbital_life": "About 10 years ( Re-entered in 1989 )" +}, +{ +"name": "Aryabhata ", +"id": 1, +"mission": "Scientific/ Experimental", +"weight": "360 kg", +"on_board_power": "46 Watts", +"communication": "VHF band", +"stabilization": "Spinstabilize", +"payload": "X-ray Astronomy Aeronomy & Solar Physics", +"launch_date": "April 19, 1975", +"launch_site": "Volgograd Launch Station (presently in Russia)", +"launch_vehicle": "C-1 Intercosmos", +"orbit": "563 x 619 km", +"inclination": "50.7 deg", +"mission_life": "6 months(nominal), Spacecraft mainframe active till March,1981", +"orbital_life": "Nearly seventeen years (Re-entered on February 10,1992)" +} +] From ace22fffacc2d0b184858deeefc60c65b2b86522 Mon Sep 17 00:00:00 2001 From: Anin Arafath Date: Sat, 15 Apr 2023 21:47:29 +0530 Subject: [PATCH 5/9] api for spacecraft missions --- api/spacecraft_missions.js | 0 data/{missions.json => spacecraft_missions.json} | 0 2 files changed, 0 insertions(+), 0 deletions(-) create mode 100644 api/spacecraft_missions.js rename data/{missions.json => spacecraft_missions.json} (100%) diff --git a/api/spacecraft_missions.js b/api/spacecraft_missions.js new file mode 100644 index 0000000..e69de29 diff --git a/data/missions.json b/data/spacecraft_missions.json similarity index 100% rename from data/missions.json rename to data/spacecraft_missions.json From 2d04bbe2edcd654d556f179784239e4a483869e3 Mon Sep 17 00:00:00 2001 From: Anin Arafath Date: Sat, 15 Apr 2023 21:51:08 +0530 Subject: [PATCH 6/9] api for space craft mission --- api/spacecraft_missions.js | 16 ++++++++++++++++ 1 file changed, 16 insertions(+) diff --git a/api/spacecraft_missions.js b/api/spacecraft_missions.js index e69de29..22ce295 100644 --- a/api/spacecraft_missions.js +++ b/api/spacecraft_missions.js @@ -0,0 +1,16 @@ +const fs = require("fs"); + +let launchers = require("../data/spacecraft_missions.json"); + +module.exports = async (req, res) => { + try { + res.send(launchers); + } catch (error) { + res.status(500); + const response = error.response || {}; + res.send({ + message: error.message, + response, + }); + } +}; From f0df559b9945e0e0259ff194fe466a810b1013ee Mon Sep 17 00:00:00 2001 From: Anin Arafath Date: Sat, 15 Apr 2023 21:55:46 +0530 Subject: [PATCH 7/9] =?UTF-8?q?=20updated=20readme=20file=20=F0=9F=A5=B3?= MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit --- README.md | 20 +++++++++----------- 1 file changed, 9 insertions(+), 11 deletions(-) diff --git a/README.md b/README.md index 2ace3c8..27fcfcf 100644 --- a/README.md +++ b/README.md @@ -1,14 +1,12 @@ -# ISRO Open Source API for Launched Spacecrafts & Rockets Data +# ISRO 🚀 API -Welcome to the ISRO Open Source API for Launched Spacecrafts & Rockets Data! This API provides access to data about ISRO spacecrafts, launchers, customer satellites, and centres. +Open Source API for Launched Spacecrafts & Rockets data of ISRO -## Endpoints - -The API provides the following endpoints: - -### Spacecrafts - -The `/api/spacecrafts` endpoint returns data about ISRO spacecrafts. The data includes the name of the spacecraft, the type of spacecraft, the launch date, and the mission details. - -Example Request: +## API End-Points +Spacecraft: [/api/spacecrafts](https://isro.vercel.app/api/spacecrafts) +- Launchers: [/api/launchers](https://isro.vercel.app/api/launchers) +- Customer Satellites: [/api/customer_satellites](https://isro.vercel.app/api/customer_satellites) +- Centres: [/api/centres](https://isro.vercel.app/api/centres) +### Mission End-Points +- Spacecraft Missions: [/api/spacecraft_missions](https://isro.vercel.app/api/spacecraft_missions) From e20ea9e6ce5222c1e5f62ad167886ca54ae34ce3 Mon Sep 17 00:00:00 2001 From: Anin Arafath Date: Sat, 15 Apr 2023 21:58:35 +0530 Subject: [PATCH 8/9] =?UTF-8?q?cleaned=20data=20space=20craft=20mission=20?= =?UTF-8?q?data=20scraped=20from=20isro's=20offical=20site=F0=9F=A5=B3?= MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit --- data/spacecraft_missions.json | 1932 ++++++++++++++++----------------- 1 file changed, 966 insertions(+), 966 deletions(-) diff --git a/data/spacecraft_missions.json b/data/spacecraft_missions.json index 72ae8e5..78e00aa 100644 --- a/data/spacecraft_missions.json +++ b/data/spacecraft_missions.json @@ -1,968 +1,968 @@ [ -{ -"name": "RISAT-2BR1", -"id": 65, -"lift-off_weight": "628 kg", -"altitude": "576 km", -"payload": "X-Band Radar", -"inclination": "37 deg", -"mission_life": "5 years" -}, -{ -"name": "Cartosat-3", -"id": 64, -"mean________________________________________________________________altitude": "509 km", -"mean_inclination": "97.5\u00b0", -"overall_mass": "1625 kg", -"power_generation": "2000W", -"mission_life": "5 years" -}, -{ -"name": "GSAT-15", -"id": 63, -"mission": "Communication and Satellite Navigation", -"weight": "3164 kg (Mass at Lift \u2013 off) 1440 kg (Dry Mass)", -"power": "Solar array providing 6200 Watts and Three 100 AH Lithium-Ion batteries", -"propulsion": "Bi- propellant System", -"launch____________________________________________________________date": "November 11, 2015", -"launch____________________________________________________________site": "Kourou, French Guiana", -"launch____________________________________________________________vehicle": "Ariane-5 VA-227", -"orbit": "Geostationary (93.5\u00b0 East longitude)Co-located with INSAT-3A and INSAT-4B", -"mission____________________________________________________________life": "12 Years" -}, -{ -"name": "GSAT-6", -"id": 62, -"physical____________________________________________________________properties": "Lift off Mass : 2117 kg Main Structure : I-2K Overall size(m) : 2.1 x 2.5 x 4.1", -"power": "Generated power 3100 W", -"aocs": "Momentum biased 3-axis stabilised", -"antennas": "One 0.8 m (fixed) and one 6 m unfurlable antenna (transmit and receive)", -"communication____________________________________________________________payloads": "i. S-band payload with five spot beams covering India for user links ii. C-band payload with one beam covering India for hub links S-band payload uses 6 m unfurlable antenna and C-band uses 0.8 m antenna.", -"mission_life": "9 years" -}, -{ -"name": "IRNSS-1B", -"id": 61, -"off_mass": "1432 kg", -"physical_dimensions": "1.58 metre x 1.50 metre x 1.50 metre", -"orbit": "Geosynchronous, at 55 deg East longitude with 29 deg inclination", -"power": "Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity", -"propulsion": "440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters", -"control_system": "Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators", -"mission_life": "10 years", -"launch_date": "Apr 04, 2014", -"launch_site": "SDSC SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV - C24" -}, -{ -"name": "GSAT-14", -"id": 60, -"mass_at_lift-off": "1982 kg", -"overall_size_(m)": "2.0 X 2.0 X 3.6", -"power": "2600 W", -"attitude_and_orbit_control_system_(aocs)": "Momentum biased 3-axis stabilized mode", -"propulsion_system": "Bi propellant-Mono Methyl Hydrazine and Mixed Oxides of Nitrogen (MON-3)", -"antennae": "One 2m and one 2.2 m single shell shaped reflector Antennae (transmit and receive)", -"launch_date": "January 05, 2014", -"launch_site": "SDSC, SHAR", -"launch_vehicle": "GSLV-D5", -"orbit": "74 deg East longitude in geostationary orbit", -"mission_life": "12 Years" -}, -{ -"name": "GSAT-7", -"id": 59, -"mission": "Communication", -"mass_at_lift-off": "2650 kg", -"physical_dimensions": "3.1 m X 1.7 m X 2.0 m", -"power": "3,000 W (end of life)", -"satbilisation": "3-axis stabilized", -"launch_date": "August 30, 2013", -"launch_site": "Kourou, French Guiana", -"launch_vehicle": "Ariane-5 VA-215", -"orbit": "74oE Geo Stationary", -"mission_life": "> 7 Years" -}, -{ -"name": "INSAT-3D", -"id": 58, -"mission": "Meteorological and Search & Rescue Services", -"mass_at_lift-off": "2060 kg", -"power": "Solar panel generating 1164 W Two 18 Ah Ni-Cd batteries", -"physical_dimensions": "2.4m x 1.6m x 1.5m", -"propulsion": "440 Newton Liquid Apogee Motor (LAM) and twelve 22 Newton thrusters with Mono Methyl Hydrazine (MMH) as fuel and mixed Oxides of Nitrogen (MON-3) as oxidizer", -"stabilisation": "3-asix body stabilized in orbit using Sun Sensors, Star Sensors, gyroscopes, Momentum and Reaction Wheels, Magnetic Torquers and thrusters", -"antennae": "0.9m and 1.0m body mounted antennas", -"launch_date": "July 26, 2013", -"launch_site": "Kourou, French Guiana", -"launch_vehicle": "Ariane-5 VA-214", -"orbit": "Geostationary, 82 deg E Longitude", -"mission_life": "7 Years" -}, -{ -"name": "IRNSS-1A", -"id": 57, -"lift-off_mass": "1425 kg", -"physical_dimensions": "1.58 metre x 1.50 metre x 1.50 metre", -"orbit": "Geosynchronous, at 55 deg East longitude with 29 deg inclination", -"power": "Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity", -"propulsion": "440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters", -"control_system": "Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators", -"mission_life": "10 years", -"launch_date": "Jul 01, 2013", -"launch_site": "SDSC SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV - C22" -}, -{ -"name": "SARAL", -"id": 56, -"lift-off_mass": "407 kg", -"orbit": "781 km polar Sun synchronous", -"sensors": "4 PI sun sensors, magnetometer, star sensors and miniaturised gyro based Inertial Reference Unit", -"orbit_inclination": "98.538o", -"local_time_of_equator": "18:00 hours crossing", -"power": "Solar Array generating 906 W and 46.8 Ampere-hour Lithium-ion battery", -"onboard_data_storage": "32 Gb", -"attitude_and_orbit_control": "3-axis stabilisation with reaction wheels, Hydrazine Control System based thrusters", -"mission_life": "5 years", -"launch_date": "Feb 25, 2013", -"launch_site": "SDSC SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV - C20" -}, -{ -"name": "GSAT-10", -"id": 55, -"mission": "Communication", -"weight": "3400 kg (Mass at Lift \u2013 off) 1498 kg (Dry Mass)", -"power": "Solar array providing 6474 Watts (at Equinox) and two 128 AH Lithium-Ion batteries", -"physical_dimensions": "2.0 m X 1.77 m X 3.1 m cuboid", -"propulsion": "440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", -"stabilisation": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", -"antennae": "East : 2.2 m dia circular deployable Dual Gridded Reflector (DGR) West : 2.2 m X 2.4 m elliptical deployable DGR Earth Viewing Face (top) : 0.7 m parabolic, 0.9 m parabolic and 0.8 m X 0.8 m sixteen element helical antenna for GAGAN", -"launch_date": "September 29, 2012", -"launch_site": "Kourou, French Guiana", -"launch_vehicle": "Ariane-5 VA-209", -"orbit": "Geostationary (83\u00b0 East longitude), co-located with INSAT-4A and GSAT-12", -"mission_life": "15 Years" -}, -{ -"name": "RISAT-1", -"id": 54, -"mass": "1858 kg", -"orbit": "Circular Polar Sun Synchronous", -"orbit_altitude": "536 km", -"orbit_inclination": "97.552o", -"orbit_period": "95.49 min", -"number_of_orbits_per_day": "14", -"local_time_of_equator_crossing": "6:00 am / 6:00 pm", -"power": "Solar Array generating 2200 W and one 70 AH Ni-H2 battery", -"repetivity": "25 days", -"attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", -"nominal_mission_life": "5 years", -"launch_date": "April 26, 2012", -"launch_site": "SDSC SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV- C19" -}, -{ -"name": "Megha-Tropiques", -"id": 53, -"lift-off_mass": "1000 kg", -"orbit": "867 km with an inclination of 20 deg to the equator", -"thermal": "Passive system with IRS heritage", -"power": "1325 W (at End of Life) Two 24 AH NiCd batteries", -"ttc": "S-band", -"attitude_and_orbit_control": "3-axis stabilised with 4 Reaction Wheels, Gyros and Star sensors, Hydrazine based RCS", -"solid_state_recorder": "16 Gb", -"launch_date": "October 12, 2011", -"launch_site": "SDSC SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV- C18" -}, -{ -"name": "GSAT-12", -"id": 52, -"mission": "Communication", -"weight": "1410 kg (Mass at Lift \u2013 off) 559 kg (Dry Mass)", -"power": "Solar array providing 1430 Watts and one 64 Ah Li-Ion batteries", -"physical_dimensions": "1.485 x 1.480 x 1.446 m cuboid", -"propulsion": "440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", -"attitude_orbit_control": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", -"antennae": "One 0.7 m diameter body mounted parabolic receive antenna and one 1.2 m diameter polarisation sensitive deployable antenna", -"launch_date": "July 15, 2011", -"launch_site": "SHAR, Sriharikota, India", -"launch_vehicle": "PSLV-C17", -"orbit": "Geosynchronous (83\u00b0 longitude)", -"mission_life": "About 8 Years" -}, -{ -"name": "GSAT-8", -"id": 51, -"mission": "Communication", -"weight": "3093 kg (Mass at Lift \u2013 off) 1426 kg (Dry Mass)", -"power": "Solar array providing 6242 watts three 100 Ah Lithium Ion batteries", -"physical_dimensions": "2.0 x 1.77 x 3.1m cuboid", -"propulsion": "440 Newton Liquid Apogee Motors (LAM) with mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", -"stabilisation": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", -"antennas": "Two indigenously developed 2.2 m diameter transmit/receive polarisation sensitive dual grid shaped beam deployable reflectors with offset-fed feeds illumination for Ku-band; 0.6 m C-band and 0.8x0.8 sq m L-band helix antenna for GAGAN", -"launch_date": "May 21, 2011", -"launch_site": "Kourou, French Guiana", -"launch_vehicle": "Ariane-5 VA-202", -"orbit": "Geosynchronous (55\u00b0 E)", -"mission_life": "More Than 12 Years" -}, -{ -"name": "RESOURCESAT-2", -"id": 50, -"mission": "Remote Sensing", -"orbit": "Circular Polar Sun Synchronous", -"orbit_altitude_at_injection": "822 km + 20 km (3 Sigma)", -"orbit_inclination": "98.731\u00ba + 0.2\u00ba", -"lift-off_mass": "1206 kg", -"orbit_period": "101.35 min", -"number_of_orbits_per_day": "14", -"local_time_of_equator_crossing": "10:30 am", -"repetivity": "24 days", -"attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", -"power": "Solar Array generating 1250 W at End Of Life, two 24 AH Ni-Cd batteries", -"launch_date": "April 20, 2011", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C16", -"mission_life": "5 years" -}, -{ -"name": "YOUTHSAT", -"id": 49, -"lift-off_mass": "92 kg", -"orbit_period": "101.35 min", -"dimension": "1020 (Pitch) x 604 (Roll) x 1340 (Yaw) mm3", -"attitude_and_orbit_control": "3-axis body stabilised using Sun and Star Sensors, Miniature Magnetometer, Miniature Gyros, Micro Reaction Wheels and Magnetic Torquers", -"power": "Solar Array generating 230 W, one 10.5 AH Li-ion battery", -"mechanisms": "Paraffin Actuator based Solar Panel Hold Down and Release Mechanism", -"launch_date": "April 20, 2011", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C16", -"orbit": "Circular Polar Sun Synchronous", -"orbit_altitude_at_injection": "822 km\u00a0+\u00a020 km (3 Sigma)", -"orbit_inclination": "98.731 \u00ba\u00a0+\u00a00.2 \u00ba", -"mission_life": "2 years" -}, -{ -"name": "CARTOSAT-2B", -"id": 48, -"mission": "Remote Sensing", -"weight": "694 kg (Mass at lift off)", -"onboard_orbit": "930 Watts", -"stabilization": "3 \u2013 axis body stabilised based on inputs from star sensors and gyros using Reaction wheels, Magnetic Torquers and Hydrazine Thrusters", -"payloads": "Panchromatic Camera", -"launch_date": "July 12, 2010", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C15", -"orbit": "630 kms, Polar Sun Synchronous", -"inclination": "97.71\u00ba" -}, -{ -"name": "Oceansat-2", -"id": 47, -"date": "Sept 23, 2009", -"launch_site": "SHAR, Sriharikota", -"launch_vehicle": "PSLV - C14", -"orbit": "Polar Sun Synchronous", -"altitude": "720 km", -"inclination": "98.28\u00b0", -"period": "99.31 minutes", -"local_time_of_eq._crossing": "12 noon \u00b1 10 minutes", -"repetitivity_cycle": "2 days", -"payloads": "OCM, SCAT and ROSA", -"mass_at_lift_off": "960 kg", -"power": "15 Sq.m Solar panels generating 1360W, Two 24 Ah Ni-Cd Batteries", -"mission_life": "5 years" -}, -{ -"name": "RISAT-2", -"id": 46, -"altitude": "550 km", -"inclination": "41 deg", -"orbit_period": "90 minutes", -"mass": "300 kg" -}, -{ -"name": "Chandrayaan-1 ", -"id": 45, -"mission": "Remote Sensing, Planetary Science", -"weight": "1380 kg (Mass at lift off)", -"onboard_power": "700 Watts", -"stabilization": "3 - axis stabilised using reaction wheel and attitude control thrusters, sun sensors, star sensors, fibre optic gyros and accelerometers for attitude determination.", -"launch_date": "22 October 2008", -"launch_site": "SDSC, SHAR, Sriharikota", -"launch_vehicle": "PSLV - C11", -"orbit": "100 km x 100 km : Lunar Orbit", -"mission_life": "2 years" -}, -{ -"name": "IMS-1", -"id": 44, -"orbit": "Polar Sun Synchronous", -"altitude": "635 km", -"mission_life": "2 years", -"physical_dimensions": "0.604x0.980x1.129 m", -"mass": "83 kg", -"power": "Two deployable sun pointing solar panels generating 220 W power, 105 Ah Lithium ion battery", -"telemetry,_tracking_and_command": "S-band", -"attitude_and_orbit_control_system": "Star Sensor, Miniature Sun Sensors, Magnetometers Gyros, Miniature Micro Reaction Wheels, Magnetic Torquers, single 1 N Hydrazine Thruster", -"data_handling": "S-band", -"data_storage": "16 Gb Solid State Recorder" -}, -{ -"name": "CARTOSAT \u2013\n2A", -"id": 43, -"mission": "Remote Sensing", -"weight": "690 Kg (Mass at lift off)", -"onboard_power": "900 Watts", -"stabilization": "3 \u2013 axis body stabilised using high torque reaction wheels, magnetic torquers and hydrogen thrusters", -"payloads": "Panchromatic Camera", -"launch_date": "28 April 2008", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C9", -"orbit": "635 km, Polar Sun Synchronous", -"inclination": "97.94 deg", -"mission_life": "5 years" -}, -{ -"name": "INSAT-4CR", -"id": 42, -"mission": "Communication", -"weight": "2,130 kg (Mass at Lift \u2013 off)", -"onboard_power": "3000 W", -"communication_payload": "12 Ku-band transponders employing 140 W Traveling Wave Tube Amplifiers (TWTA) Ku-band Beacon", -"launch_date": "September 2, 2007", -"launch_site": "SHAR, Sriharikota, India", -"launch_vehicle": "GSLV-F04", -"orbit": "Geosynchronous (74\u00b0 E)", -"mission_life": "12 Years" -}, -{ -"name": "INSAT-4B", -"id": 41, -"mission": "Communication", -"weight": "3025 kg (at Lift \u2013 off)", -"onboard_power": "5859 W", -"stabilization": "It uses 3 earth sensors, 2 digital sun sensors, 8 coarse analog sun sensors, 3 solar panel sun sensors and one sensor processing electronics. The wheels and wheel drive electronics were imported with indigenous wheel interface module to interface the wheel drive electronics and AOCE.", -"propulsion": "The propulsion system is employing 16 thrusters, 4 each located on east, west and AY sides and 2 each on north and south sides. There is one 440 N liquid apogee motor (using Mono Methyl Hydrazine (MMH) as fuel and oxides of Nitrogen (MON3 as oxidizer) and three pressurant tanks mounted on the LAM deck.", -"payload": "12 Ku band high power transponders covering Indian main land using 140W radiatively cooled TWTAs.", -"launch_date": "March 12, 2007", -"launch_site": "French Guiana", -"launch_vehicle": "Ariane5", -"orbit": "Geostationary (93.5o E Longitude)", -"mission_life": "12 Years" -}, -{ -"name": "CARTOSAT-2", -"id": 40, -"mission": "Remote Sensing", -"weight": "650 Kg", -"onboard_orbit": "900 Watts", -"stabilization": "3 - axis body stabilised using high torque reaction wheels, magnetic torquers and thrusters", -"payloads": "Panchromatic Camera", -"launch_date": "10 January 2007", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C7", -"orbit": "Polar Sun Synchronous", -"mission_life": "5 years" -}, -{ -"name": "INSAT-4A", -"id": 39, -"spacecraft_mass": "Lift off 3081 Kg Dry Mass 1386.55 Kg", -"orbit": "Geostationary ( 83o E)", -"power": "Solar Array to provide a power of 5922 W", -"battery": "Three 70 Ah Ni H2 Batteries for eclipse support of 4264 W", -"life": "12 Years", -"launch_date": "December 22, 2005", -"launch_vehicle": "ARIANE5-V169" -}, -{ -"name": "CARTOSAT-1", -"id": 38, -"launch_date": "5 May 2005", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C6", -"orbit": "618 km Polar Sun Synchronous", -"payloads": "PAN FORE, PAN - AFT", -"orbit_period": "97 min", -"number_of_orbits_per_day": "14", -"local_time_of_equator_crossing": "10:30 am", -"repetivity": "126 days", -"revisit": "5 days", -"lift-off_mass": "1560 kg", -"attitude_and_orbit_control": "3-axis body stabillised using reaction wheels, Magnetic Torquers and Hydrazine Thrusters", -"electrical_power": "15 sqm Solar Array generating 1100w, Two 24 Ah Ni-Cd batteries", -"mission_life": "5 years" -}, -{ -"name": "HAMSAT", -"id": 37, -"launch_date": "May 5, 2005", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV-C6", -"orbit": "Geo-synchronous, 633.355 km (average)", -"payloads": "2 Transponders" -}, -{ -"name": "EDUSAT", -"id": 36, -"mission": "Education", -"spacecraft_mass": "1950.5 kg mass (at Lift - off) 819.4 kg (Dry mass)", -"onboard_power": "Total four solar panel of size 2.54 M x 1.525 M generating 2040 W (EOL), two 24 AH NiCd batteries for eclipse support", -"stabilization": "3 axis body stabilised in orbit using sensors, momentum and reaction wheels, magnetic torquers and eight 10 N & 22N reaction control thrusters.", -"propulsion": "440 N Liquid Apogee Motor with MON - 3 and MMH for orbit raising", -"payload": "Six upper extended C - band transpondersFive lower Ku band transponders with regional beam coverage One lower Ku band National beam transponder with Indian main land coverageKu beacon12 C band high power transponders with extended coverage, covering southeast and northwest region apart from Indian main land using 63 W LTWTAs", -"launch_date": "September 20, 2004", -"launch_site": "SHAR, Sriharikota, India", -"launch_vehicle": "GSLV-F01", -"orbit": "Geostationary (74oE longitude)", -"mission_life": "7 Years (minimum)" -}, -{ -"name": "IRS-P6 / RESOURCESAT-1", -"id": 35, -"launch_date": "October 17, 2003", -"launch_site": "SHAR, Sriharikota", -"launch_vehicle": "PSLV-C5", -"payloads": "LISS-4, LISS-3, AWiFS-A, AWiFS-B", -"orbit": "Polar Sun Synchronous", -"orbit_height": "817 km", -"orbit_inclination": "98.7o", -"orbit_period": "101.35 min", -"number_of_orbits_per_day": "14", -"local_time_of_equator_crossing": "10:30 am", -"repetivity_(liss-3)": "24 days", -"revisit": "5 days", -"lift-off_mass": "1360 kg", -"attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", -"power": "Solar Array generating 1250 W, Two 24 Ah Ni-Cd batteries", -"mission_life": "5 years" -}, -{ -"name": "INSAT-3E", -"id": 34, -"mission": "Communication", -"spacecraft_mass": "2,775 kg (Mass at Lift-off) 1218 kg (Dry mass)", -"launch_date": "September 28, 2003", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane5-V162", -"orbit": "Geostationary Orbit" -}, -{ -"name": "GSAT-2", -"id": 33, -"mission": "Communication", -"weight": "1800 kg", -"launch_date": "May 8, 2003", -"launch_site": "SHAR, Sriharikota, India", -"launch_vehicle": "GSLV\u2013D2", -"orbit": "Geostationary orbit (48oE longitude)" -}, -{ -"name": "INSAT-3A", -"id": 32, -"mission": "Telecommunication, broadcasting and Meteorology", -"spacecraft_mass": "2,950 kg (Mass at Lift\u2013off) 1,348 kg (Dry mass)", -"onboard_power": "3,100 W", -"stabilization": "3 \u2013 axis body stabilised in orbit using momentum and reaction wheels, solar flaps, magnetic torquers and eight 10 N and eight 22 N reaction control thrusters", -"propulsion": "440 N Liquid Apogee Motor with MON-3 (Mixed Oxides of Nitrogen) and MMH (Mono Methyl Hydrazine) for orbit raising", -"payload": "Communication payload- 12 C \u2013 band transponders, - 6 upper extended C band transponders - 6 Ku band transponders - 1 Satellite Aided Search & Rescue transponders Meteorological payload- Very High Resolution Radiometer (VHRR) with 2 km resolution in visible band and 8 km resolution in infrared and water vapour band- Charged Coupled Device (CCD) camera operating in visible, near infrared and shortwave infrared band with 1 km resolution.- Data Relay Transponders (DRT)", -"launch_date": "April 10, 2003", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane5-V160", -"orbit": "Geostationary (93.5o E longitude)", -"mission_life": "12 Years" -}, -{ -"name": "KALPANA-1", -"id": 31, -"mission": "7 Years", -"spacecraft_mass": "1060 kg mass (at Lift \u2013 off) 498 kg (Dry mass)", -"onboard_power": "550 W", -"payload": "Very High Resolution Radiometer (VHRR) Data Relay Transponder (DRT)", -"launch_date": "12 September 2002", -"launch_site": "SHAR, Sriharikota", -"launch_vehicle": "PSLV \u2013 C4", -"orbit": "Geostationary (74 deg East longitude)" -}, -{ -"name": "INSAT-3C", -"id": 30, -"mission": "Communication, broadcasting and Meteorology", -"spacecraft_mass": "2,650 kg (Mass at Lift - off) 1218 kg (Dry mass)", -"onboard_power": "2765 W", -"propulsion": "Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.", -"payload": "24 C band transponders 6 Extended C - band Transponders 2 S - band Transponders", -"launch_date": "January 24, 2002", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane5-V147", -"orbit": "Geostationary (74o longitude)", -"mission_life": "Very long" -}, -{ -"name": "The Technology Experiment Satellite\n(TES)", -"id": 29, -"launch_date": "22 October 2001", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C3", -"orbit": "572 km Sun Synchronous", -"payloads": "PAN" -}, -{ -"name": "PSLV-C3 / TES", -"id": 28, -"launch_date": "22 October 2001", -"launch_site": "SHAR Centre Sriharikota India", -"launch_vehicle": "PSLV- C3", -"orbit": "572 km Sun Synchronous", -"payloads": "PAN" -}, -{ -"name": "GSAT-1", -"id": 27, -"mission": "Communication", -"weight": "1530 kg", -"launch_date": "18 April 2001", -"launch_site": "SHAR, Sriharikota", -"launch_vehicle": "GSLV \u2013 D1", -"orbit": "Sun Synchronous Geo stationary orbit" -}, -{ -"name": "INSAT-3B", -"id": 26, -"mission": "Very long", -"spacecraft_mass": "2,070 (Mass at Lift \u2013 off) 970 kg (Dry mass)", -"onboard_power": "1,712 W", -"stabilization": "3 \u2013 axis body stabilised biased momentum control system using earth sensors, sun sensors, inertial reference unit, momentum / reaction wheels, magnetic torquers and unified bi-propellant thrusters.", -"propulsion": "Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.", -"payload": "12 extended C \u2013 band Transponders Five Ku band Transponders Mobile Satellite Services (MSS)", -"launch_date": "22nd March 2000", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane -5", -"orbit": "Geostationary (83 deg East longitude)", -"inclination": "7 deg" -}, -{ -"name": "Oceansat(IRS-P4)", -"id": 25, -"launch_date": "May 26, 1999", -"launch_site": "SHAR, Sriharikota", -"launch_vehicle": "PSLV - C2", -"orbit": "Polar Sun Synchronous", -"altitude": "720 km", -"inclination": "98.28 deg", -"period": "99.31 min", -"local_time_of_eq._crossing": "12 noon", -"repetitivity_cycle": "2 days", -"size": "2.8m x 1.98m x 2.57m", -"mass_at_lift_off": "1050 kg", -"length_when_fully_deployed": "11.67 m", -"attitude_and_orbit_control": "3-axis body-stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", -"power": "9.6 Sq.m Solar Array generating 750w Two 21 Ah Ni-Cd Batteries", -"mission_completed_on": "August 8, 2010" -}, -{ -"name": "INSAT-2E", -"id": 24, -"mission": "Communication and Meteorology", -"spacecraft_mass": "2,550 kg (Mass at Lift-off) 1150 kg (Dry mass)", -"launch_date": "03 April 1999", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane \u2013 42P", -"orbit": "Geosynchronous (83 deg east longitude)" -}, -{ -"name": "IRS-1D", -"id": 23, -"mission": "Operational Remote Sensing", -"weight": "1250 kg", -"onboard_power": "809 Watts (generated by 9.6 sq.metres Solar Panels)", -"communication": "S-band, X-band", -"stabilization": "Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer", -"rcs": "Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters", -"payload": "Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)", -"onboard_tape_recorder": "Storage Capacity : 62 G bits", -"launch_date": "December 28, 1995", -"launch_site": "Baikanur Cosmodrome Kazakhstan", -"launch_vehicle": "Molniya", -"orbit": "817 km Polar Sun-synchronous", -"inclination": "98.69o", -"repetivity": "24 days", -"local_time": "10.30 a.m", -"mission_completed_on": "September 21, 2007" -}, -{ -"name": "INSAT-2D", -"id": 22, -"mission": "Communication", -"weight": "2079 kg with propellants, 995 kg dry weight", -"onboard_power": "1650 Watts", -"communication": "C, extended C, S and Ku bands", -"stabilization": "Three axis stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", -"propulsion": "Integrated bipropellan stystem ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.", -"payload": "Transponders: 16C-band / extended C-band transponders (forFSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders", -"launch_date": "June 4, 1997", -"launch_site": "French Guyana", -"launch_vehicle": "Arianev 4", -"orbit": "Geostationary 93,.5deg.E", -"inclination": "0 deg." -}, -{ -"name": "IRS-P3", -"id": 21, -"mission": "Remote sensing of earth's natural resources. Study of X-ray Astronomy. Periodic calibration of PSLV tracking radar located at tracking stations.", -"weight": "920 kg", -"onboard_power": "817 Watts", -"communication": "S-band", -"stabilization": "Three axis body stabilized", -"rcs": "Combinations of bladder type and surface tension type mass expulsion monopropellant hydrazine system", -"payload": "WideField Sensor (WiFS), Modular Opto - electronic Scanner (MOS), Indian X-ray Astronomy Experiment (IXAE), C-band transponder(CBT)", -"launch_date": "March 21, 1996", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV-D3", -"orbit": "817 km. Circular polar sun-synchronous with equatorial crossing at 10.30 am (descending node)", -"inclination": "98.68o", -"repetivity": "WiFS : 5 days", -"mission_completed_during": "January 2006" -}, -{ -"name": "IRS-1C", -"id": 20, -"mission": "Operational Remote Sensing", -"weight": "1250 kg", -"onboard_power": "809 Watts (generated by 9.6 sq.metres Solar Panels)", -"communication": "S-band, X-band", -"stabilization": "Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer", -"rcs": "Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters", -"payload": "Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)", -"onboard_tape_recorder": "Storage Capacity : 62 G bits", -"launch_date": "December 28, 1995", -"launch_site": "Baikanur Cosmodrome Kazakhstan", -"launch_vehicle": "Molniya", -"orbit": "817 km Polar Sun-synchronous", -"inclination": "98.69o", -"repetivity": "24 days", -"local_time": "10.30 a.m", -"mission_completed_on": "September 21, 2007" -}, -{ -"name": "INSAT-2C", -"id": 19, -"mission": "Communication", -"weight": "2106 kg with propellants 946 kg dry weight", -"onboard_power": "1320 Watts", -"communication": "C extended C, S and Ku bands", -"stabilization": "Three axis stabilized with two Momen'tum Wheels & one Reaction Wheel, Magnetic torquers", -"propulsion": "Integrated bipropellant system ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.", -"payload": "Transponders: 16C-band / extended C-band transponders (for FSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders", -"launch_date": "December 7, 1995", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane4", -"orbit": "Geostationary 93.5 deg E", -"inclination": "0 deg.", -"mission_life": "Seven years(nominal)", -"orbit_life": "Very Long" -}, -{ -"name": "IRS-P2", -"id": 18, -"mission": "Operational Remote Sensing", -"weight": "804 kg", -"onboard_power": "510 Watts", -"communication": "S-band, X-band", -"stabilization": "Three axis body stabilized with 4 Reaction Wheels, Magnetic torquers", -"rcs": "4 tanks containing Monopropellant Hydrazine based with sixteen 1 N thrusters and one 11 N thruster", -"payload": "Two solid state Push Broom Cameras operating in four spectral bands in the visible and near-IR range using CCD arrays: LlSS-2A & LlSS-2B (Resolution: 32.74 metre)", -"launch_date": "October 15, 1994", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV-D2", -"inclination": "98.68o", -"repetivity": "24 days", -"mission_completed_on": "1997" -}, -{ -"name": "SROSS-C2", -"id": 17, -"mission": "Experimental", -"weight": "115 kg", -"onboard_power": "45 Watts", -"communication": "S-band and VHF", -"rcs": "Monopropellant Hydrazine based with six 1 Newton thrusters", -"payload": "Gamma Ray Burst (GRB) & Retarding Potential Analyser (RPA)", -"launch_date": "May 04,1994", -"launch_site": "SHAR Centre,Sriharikota,India", -"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", -"orbit": "430 x 600 km.", -"inclination": "45 deg.", -"mission_life": "Six months (nominal)", -"orbital_life": "Two years (nominal)" -}, -{ -"name": "IRS-1E", -"id": 16, -"mission": "Operational Remote Sensing", -"weight": "846 kg", -"onboard_power": "415 Watts", -"communication": "S-band (TIC) & VHF", -"stabilization": "Three axis body stabilized ( zero momentum) with 4 Reaction Wheels, Magnetic torquers", -"rcs": "Monopropellant Hydrazine based RCS with 1 Newton thrusters ( 16 Nos.)", -"payload": "LlSS-1 MEOSS (Mono-ocula Erlectro Optic Stereo Scanner)", -"launch_date": "September 20, 1993", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "PSLV-D1", -"orbit": "Not realised" -}, -{ -"name": "INSAT-2B", -"id": 15, -"mission": "Multipurpose Communication, meteorology and Satellite based search and rescue", -"weight": "1906 kg with propellant 916 kg dry weight", -"onboard_power": "One KW approx.", -"communication": "C, extended C and S band", -"stabilization": "Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", -"propulsion": "Integrated bipropellant system ( MMH and N2 04) With sixteen 22 N thrusters and 440 N LAM.", -"payload": "Transponders: 12C-band (for FSS),6 ext. C-band (for FSS) 2S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band", -"launch_date": "July 23, 1993", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane 4", -"orbit": "Geostationary 93.5o E", -"inclination": "0o", -"mission_life": "Seven years(nominal)", -"orbit_life": "Very Long" -}, -{ -"name": "INSAT-2A", -"id": 14, -"mission": "Multipurpose Communication, meteorology and Satellite based search and rescue", -"weight": "1906 kg with propellant 916 kg dry weight", -"onboard_power": "One KW approx", -"communication": "C, extended C and S band", -"stabilization": "Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", -"propulsion": "Integrated bipropellant system (MMH and N2 04) With sixteen 22 N thrusters and 440 LAM.", -"payload": "Transponders: 12 C-band (for FSS),6 ext. C-band (for FSS) 2 S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band", -"launch_date": "July 10,1992", -"launch_site": "French Guyana", -"launch_vehicle": "Ariane 4", -"orbit": "Geostationary 74oE longitude", -"inclination": "0o", -"mission_life": "Seven years(nominal)", -"orbit_life": "Very Long" -}, -{ -"name": "SROSS-C\n", -"id": 13, -"mission": "Experimental", -"weight": "106.1 kg", -"onboard_power": "45 Watts", -"communication": "S-band and VHF", -"stabilization": "Spin stabilized with a Magnetic Torquer and Magnetic Bias Control", -"payload": "Gamma Ray Burst (GRB) experiment & Retarding Potential Analyser (RPA) experiment", -"launch_date": "May 20,1992", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", -"orbit": "267 x 391 km", -"mission_life": "Two months (Re-entered on July15,1992)" -}, -{ -"name": "IRS-1B", -"id": 12, -"mission": "Operational Remote Sensing", -"weight": "975 kg", -"onboard_power": "600 Watts", -"communication": "S-band, X-band and VHF (commanding only)", -"stabilization": "Three axis body stabilized (zero momentum) with 4 Reactions Wheels, Magnetic torquers", -"rcs": "Monopropellant Hydrazine based with sixteen 1 Newton thrusters", -"payload": "Three solid state Push Broom Cameras LlSS-1 (72.5 metre resolution), LlSS-2A and LlSS-2B (36.25 metre resolution)", -"launch_date": "August 29, 1991", -"launch_site": "Baikanur Cosmodrome Kazakhstan", -"launch_vehicle": "Vostok", -"orbit": "904 km Polar Sun Synchronous", -"inclination": "99.08o", -"repetivity": "22 days", -"local_time": "10.30 a.m. (descending node)", -"mission_completed_on": "December 20, 2003" -}, -{ -"name": "SROSS-2", -"id": 11, -"mission": "Experimental", -"weight": "150 kg", -"onboard_power": "90 Watts", -"communication": "S-band and VHF", -"stabilization": "Three axis body stabilized (biased momentum) with a MomentumWheel and Magnetic Torquer", -"propulsion_system": "Monopropellant (Hydrazine based) Reaction Control System", -"payload": "Gamma Ray Burst (GRB) payload and Mono PayloadOcular Electro-Optic Stereo Scanner (MEOSS) built by DLR, Germany", -"launch_date": "July 13, 1988", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", -"orbit": "Not realised" -}, -{ -"name": "IRS-1A", -"id": 10, -"mission": "Operational Remote Sensing", -"weight": "975 kg", -"onboard_power": "600 Watts", -"communication": "S-band, X-band and VHF(commanding only)", -"stabilization": "Three axis body stabilized (zero momentum)with 4 Reactions Wheels, Magnetic torquers", -"rcs": "Monopropellant Hydrazine based with sixteen 1 Newton thrusters", -"payload": "Three solid state Push Broom Cameras: LISS-1(72.5 metre resolution),LISS-2A and LISS-2B (36.25 metre resolution)", -"launch_date": "March 17, 1988", -"launch_site": "Baikanur Cosmodrome Kazakhstan", -"launch_vehicle": "Vostok", -"orbit": "904 km Polar Sun-synchronous", -"inclination": "99.08o", -"repetivity": "22 days (307 orbits)", -"local_time": "10.30 a.m. (descending node)", -"mission_completed_during": "July 1996" -}, -{ -"name": "SROSS-1\n", -"id": 9, -"mission": "Experimental", -"weight": "150 kg", -"onboard_power": "90 Watts", -"communication": "S-band and VHF", -"stabilization": "Three axis body stabilized (biased momentum) with a Momentum Wheel and Magnetic Torquer", -"propulsion_system": "Monopropellant (Hydrazine based) Reaction control system", -"payload": "Launch Vehicle Monitoring Platform(LVMP), Gamma Ray Burst (GRB) payload and Corner Cube Retro Reflector (CCRR) for laser tracking", -"launch_date": "March 24, 1987", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", -"orbital_life": "Not realised" -}, -{ -"name": "Rohini Satellite RS-D2", -"id": 8, -"mission": "Experimental", -"weight": "41.5 kg", -"onboard_power": "16 Watts", -"communication": "VHF band", -"stabilization": "Spin stabilized", -"payload": "Smart sensor (remote sensing payload),L-band beacon", -"launch_date": "April 17, 1983", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "SLV-3", -"orbit": "371 x 861 km", -"inclination": "46o", -"mission_life": "17 months", -"orbital_life": "Seven years (Re-entered on April 19, 1990)" -}, -{ -"name": "Bhaskara-II", -"id": 7, -"mission": "Experimental Remote Sensing", -"weight": "444 kg", -"onboard_power": "47 Watts", -"communication": "VHF band", -"stabilization": "Spin stabilized (spin axis controlled)", -"payload": "TV cameras, three band Microwave Radiometer (SAMIR)", -"launch_date": "Nov 20, 1981", -"launch_site": "Volgograd Launch Station (presently in Russia)", -"launch_vehicle": "C-1 Intercosmos", -"orbit": "541 x 557 km", -"inclination": "50.7o", -"mission_life": "One year (nominal)", -"orbital_life": "About 10 years ( Re-entered in 1991 )" -}, -{ -"name": "APPLE", -"id": 6, -"mission": "Experimental geostationary communication", -"weight": "670 kg", -"onboard_power": "210 Watts", -"communication": "VHF and C-band", -"stabilization": "Three axis stabilized (biased momentum) with Momentum Wheels, Torquers & Hydrazine based Reaction control system", -"payload": "C - band transponders (Two)", -"launch_date": "June19,1981", -"launch_site": "Kourou (CSG), French Guyana", -"launch_vehicle": "Ariane -1(V-3)", -"orbit": "Geosynchronous (102 deg. E longitude, over Indonesia)", -"inclination": "Near zero", -"mission_life": "Two years" -}, -{ -"name": "Rohini Satellite RS-D1", -"id": 5, -"mission": "Experimental", -"weight": "38 kg", -"onboard_power": "16 Watts", -"communication": "VHF band", -"stabilization": "Spin stabilized", -"payload": "Landmark Tracker ( remote sensing payload)", -"launch_date": "May 31,1981", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "SLV-3", -"orbit": "186 x 418 km (achieved)", -"inclination": "46 deg", -"orbital_life": "Nine days" -}, -{ -"name": "Rohini Satellite RS-1", -"id": 4, -"mission": "Experimental", -"weight": "35 kg", -"onboard_power": "16 Watts", -"communication": "VHF band", -"stabilization": "Spin stabilized", -"payload": "Launch vehicle monitoring instruments", -"launch_date": "July 18,1980", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "SLV-3", -"orbit": "305 x 919 km", -"inclination": "44.7 deg.", -"mission_life": "1.2 years", -"orbital_life": "20 months" -}, -{ -"name": "Rohini Technology Payload (RTP)", -"id": 3, -"mission": "Experimental", -"weight": "35 kg", -"onboard_power": "3 Watts", -"communication": "VHF band", -"stabilization": "Spin stabilized (spin axis controlled)", -"payload": "Launch vehicle monitoring instruments", -"launch_date": "August 10,1979", -"launch_site": "SHAR Centre, Sriharikota, India", -"launch_vehicle": "SLV-3", -"orbit": "Not achieved" -}, -{ -"name": "Bhaskara-I", -"id": 2, -"mission": "Experimental Remote Sensing", -"weight": "442 kg", -"onboard_power": "47 Watts", -"communication": "VHF band", -"stabilization": "Spin stabilized (spin axis controlled)", -"payload": "TVcameras, three band Microwave Radiometer (SAMIR)", -"launch_date": "Jun 07,1979", -"launch_site": "Volgograd Launch Station (presently in Russia)", -"launch_vehicle": "C-1Intercosmos", -"orbit": "519 x 541 km", -"inclination": "50.6 deg", -"mission_life": "One year (nominal)", -"orbital_life": "About 10 years ( Re-entered in 1989 )" -}, -{ -"name": "Aryabhata ", -"id": 1, -"mission": "Scientific/ Experimental", -"weight": "360 kg", -"on_board_power": "46 Watts", -"communication": "VHF band", -"stabilization": "Spinstabilize", -"payload": "X-ray Astronomy Aeronomy & Solar Physics", -"launch_date": "April 19, 1975", -"launch_site": "Volgograd Launch Station (presently in Russia)", -"launch_vehicle": "C-1 Intercosmos", -"orbit": "563 x 619 km", -"inclination": "50.7 deg", -"mission_life": "6 months(nominal), Spacecraft mainframe active till March,1981", -"orbital_life": "Nearly seventeen years (Re-entered on February 10,1992)" -} + { + "name": "RISAT-2BR1", + "id": 65, + "lift-off_weight": "628 kg", + "altitude": "576 km", + "payload": "X-Band Radar", + "inclination": "37 deg", + "mission_life": "5 years" + }, + { + "name": "Cartosat-3", + "id": 64, + "mean_altitude": "509 km", + "mean_inclination": "97.5\u00b0", + "overall_mass": "1625 kg", + "power_generation": "2000W", + "mission_life": "5 years" + }, + { + "name": "GSAT-15", + "id": 63, + "mission": "Communication and Satellite Navigation", + "weight": "3164 kg (Mass at Lift \u2013 off) 1440 kg (Dry Mass)", + "power": "Solar array providing 6200 Watts and Three 100 AH Lithium-Ion batteries ", + "propulsion": "Bi- propellant System", + "launch_date": "November 11, 2015", + "launch_site": "Kourou, French Guiana", + "launch_vehicle": "Ariane-5 VA-227", + "orbit": "Geostationary (93.5\u00b0 East longitude)Co-located with INSAT-3A and INSAT-4B", + "mission_life": "12 Years" + }, + { + "name": "GSAT-6", + "id": 62, + "physical_properties": "Lift off Mass : 2117 kg Main Structure : I-2K Overall size(m) : 2.1 x 2.5 x 4.1", + "power": "Generated power 3100 W", + "aocs": "Momentum biased 3-axis stabilised", + "antennas": "One 0.8 m (fixed) and one 6 m unfurlable antenna (transmit and receive)", + "communication_payloads": "i. S-band payload with five spot beams covering India for user links ii. C-band payload with one beam covering India for hub links S-band payload uses 6 m unfurlable antenna and C-band uses 0.8 m antenna.", + "mission_life": "9 years" + }, + { + "name": "IRNSS-1B", + "id": 61, + "off_mass": "1432 kg", + "physical_dimensions": "1.58 metre x 1.50 metre x 1.50 metre", + "orbit": "Geosynchronous, at 55 deg East longitude with 29 deg inclination", + "power": "Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity", + "propulsion": "440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters", + "control_system": "Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators", + "mission_life": "10 years", + "launch_date": "Apr 04, 2014", + "launch_site": "SDSC SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV - C24" + }, + { + "name": "GSAT-14", + "id": 60, + "mass_at_lift-off": "1982 kg", + "overall_size_(m)": "2.0 X 2.0 X 3.6", + "power": "2600 W", + "attitude_and_orbit_control_system_(aocs)": "Momentum biased 3-axis stabilized mode", + "propulsion_system": "Bi propellant-Mono Methyl Hydrazine and Mixed Oxides of Nitrogen (MON-3)", + "antennae": "One 2m and one 2.2 m single shell shaped reflector Antennae (transmit and receive)", + "launch_date": "January 05, 2014", + "launch_site": "SDSC, SHAR", + "launch_vehicle": "GSLV-D5", + "orbit": "74 deg East longitude in geostationary orbit", + "mission_life": "12 Years" + }, + { + "name": "GSAT-7", + "id": 59, + "mission": "Communication", + "mass_at_lift-off": "2650 kg", + "physical_dimensions": "3.1 m X 1.7 m X 2.0 m", + "power": "3,000 W (end of life)", + "satbilisation": "3-axis stabilized", + "launch_date": "August 30, 2013", + "launch_site": "Kourou, French Guiana", + "launch_vehicle": "Ariane-5 VA-215", + "orbit": "74oE Geo Stationary", + "mission_life": "> 7 Years" + }, + { + "name": "INSAT-3D", + "id": 58, + "mission": "Meteorological and Search & Rescue Services", + "mass_at_lift-off": "2060 kg", + "power": "Solar panel generating 1164 W Two 18 Ah Ni-Cd batteries", + "physical_dimensions": "2.4m x 1.6m x 1.5m", + "propulsion": "440 Newton Liquid Apogee Motor (LAM) and twelve 22 Newton thrusters with Mono Methyl Hydrazine (MMH) as fuel and mixed Oxides of Nitrogen (MON-3) as oxidizer", + "stabilisation": "3-asix body stabilized in orbit using Sun Sensors, Star Sensors, gyroscopes, Momentum and Reaction Wheels, Magnetic Torquers and thrusters", + "antennae": "0.9m and 1.0m body mounted antennas", + "launch_date": "July 26, 2013", + "launch_site": "Kourou, French Guiana", + "launch_vehicle": "Ariane-5 VA-214", + "orbit": "Geostationary, 82 deg E Longitude", + "mission_life": "7 Years" + }, + { + "name": "IRNSS-1A", + "id": 57, + "lift-off_mass": "1425 kg", + "physical_dimensions": "1.58 metre x 1.50 metre x 1.50 metre", + "orbit": "Geosynchronous, at 55 deg East longitude with 29 deg inclination", + "power": "Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity", + "propulsion": "440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters", + "control_system": "Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators", + "mission_life": "10 years", + "launch_date": "Jul 01, 2013", + "launch_site": "SDSC SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV - C22" + }, + { + "name": "SARAL", + "id": 56, + "lift-off_mass": "407 kg", + "orbit": "781 km polar Sun synchronous", + "sensors": "4 PI sun sensors, magnetometer, star sensors and miniaturised gyro based Inertial Reference Unit", + "orbit_inclination": "98.538o", + "local_time_of_equator": "18:00 hours crossing", + "power": "Solar Array generating 906 W and 46.8 Ampere-hour Lithium-ion battery", + "onboard_data_storage": "32 Gb", + "attitude_and_orbit_control": "3-axis stabilisation with reaction wheels, Hydrazine Control System based thrusters", + "mission_life": "5 years", + "launch_date": "Feb 25, 2013", + "launch_site": "SDSC SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV - C20" + }, + { + "name": "GSAT-10", + "id": 55, + "mission": "Communication", + "weight": "3400 kg (Mass at Lift \u2013 off) 1498 kg (Dry Mass)", + "power": "Solar array providing 6474 Watts (at Equinox) and two 128 AH Lithium-Ion batteries", + "physical_dimensions": "2.0 m X 1.77 m X 3.1 m cuboid", + "propulsion": "440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", + "stabilisation": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", + "antennae": "East : 2.2 m dia circular deployable Dual Gridded Reflector (DGR) West : 2.2 m X 2.4 m elliptical deployable DGR Earth Viewing Face (top) : 0.7 m parabolic, 0.9 m parabolic and 0.8 m X 0.8 m sixteen element helical antenna for GAGAN", + "launch_date": "September 29, 2012", + "launch_site": "Kourou, French Guiana", + "launch_vehicle": "Ariane-5 VA-209", + "orbit": "Geostationary (83\u00b0 East longitude), co-located with INSAT-4A and GSAT-12", + "mission_life": "15 Years" + }, + { + "name": "RISAT-1", + "id": 54, + "mass": "1858 kg", + "orbit": "Circular Polar Sun Synchronous", + "orbit_altitude": "536 km", + "orbit_inclination": "97.552o", + "orbit_period": "95.49 min", + "number_of_orbits_per_day": "14", + "local_time_of_equator_crossing": "6:00 am / 6:00 pm", + "power": "Solar Array generating 2200 W and one 70 AH Ni-H2 battery", + "repetivity": "25 days", + "attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", + "nominal_mission_life": "5 years", + "launch_date": "April 26, 2012", + "launch_site": "SDSC SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV- C19" + }, + { + "name": "Megha-Tropiques", + "id": 53, + "lift-off_mass": "1000 kg", + "orbit": "867 km with an inclination of 20 deg to the equator", + "thermal": "Passive system with IRS heritage", + "power": "1325 W (at End of Life) Two 24 AH NiCd batteries", + "ttc": "S-band", + "attitude_and_orbit_control": "3-axis stabilised with 4 Reaction Wheels, Gyros and Star sensors, Hydrazine based RCS", + "solid_state_recorder": "16 Gb", + "launch_date": "October 12, 2011", + "launch_site": "SDSC SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV- C18" + }, + { + "name": "GSAT-12", + "id": 52, + "mission": "Communication", + "weight": "1410 kg (Mass at Lift \u2013 off) 559 kg (Dry Mass)", + "power": "Solar array providing 1430 Watts and one 64 Ah Li-Ion batteries", + "physical_dimensions": "1.485 x 1.480 x 1.446 m cuboid", + "propulsion": "440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", + "attitude_orbit_control": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", + "antennae": "One 0.7 m diameter body mounted parabolic receive antenna and one 1.2 m diameter polarisation sensitive deployable antenna", + "launch_date": "July 15, 2011", + "launch_site": "SHAR, Sriharikota, India", + "launch_vehicle": "PSLV-C17", + "orbit": "Geosynchronous (83\u00b0 longitude)", + "mission_life": "About 8 Years" + }, + { + "name": "GSAT-8", + "id": 51, + "mission": "Communication", + "weight": "3093 kg (Mass at Lift \u2013 off) 1426 kg (Dry Mass)", + "power": "Solar array providing 6242 watts three 100 Ah Lithium Ion batteries", + "physical_dimensions": "2.0 x 1.77 x 3.1m cuboid", + "propulsion": "440 Newton Liquid Apogee Motors (LAM) with mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.", + "stabilisation": "3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters", + "antennas": "Two indigenously developed 2.2 m diameter transmit/receive polarisation sensitive dual grid shaped beam deployable reflectors with offset-fed feeds illumination for Ku-band; 0.6 m C-band and 0.8x0.8 sq m L-band helix antenna for GAGAN", + "launch_date": "May 21, 2011", + "launch_site": "Kourou, French Guiana", + "launch_vehicle": "Ariane-5 VA-202", + "orbit": "Geosynchronous (55\u00b0 E)", + "mission_life": "More Than 12 Years" + }, + { + "name": "RESOURCESAT-2", + "id": 50, + "mission": "Remote Sensing", + "orbit": "Circular Polar Sun Synchronous", + "orbit_altitude_at_injection": "822 km + 20 km (3 Sigma)", + "orbit_inclination": "98.731\u00ba + 0.2\u00ba", + "lift-off_mass": "1206 kg", + "orbit_period": "101.35 min", + "number_of_orbits_per_day": "14", + "local_time_of_equator_crossing": "10:30 am", + "repetivity": "24 days", + "attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", + "power": "Solar Array generating 1250 W at End Of Life, two 24 AH Ni-Cd batteries", + "launch_date": "April 20, 2011", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C16", + "mission_life": "5 years" + }, + { + "name": "YOUTHSAT", + "id": 49, + "lift-off_mass": "92 kg", + "orbit_period": "101.35 min", + "dimension": "1020 (Pitch) x 604 (Roll) x 1340 (Yaw) mm3", + "attitude_and_orbit_control": "3-axis body stabilised using Sun and Star Sensors, Miniature Magnetometer, Miniature Gyros, Micro Reaction Wheels and Magnetic Torquers", + "power": "Solar Array generating 230 W, one 10.5 AH Li-ion battery", + "mechanisms": "Paraffin Actuator based Solar Panel Hold Down and Release Mechanism", + "launch_date": "April 20, 2011", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C16", + "orbit": "Circular Polar Sun Synchronous", + "orbit_altitude_at_injection": "822 km\u00a0+\u00a020 km (3 Sigma)", + "orbit_inclination": "98.731 \u00ba\u00a0+\u00a00.2 \u00ba", + "mission_life": "2 years" + }, + { + "name": "CARTOSAT-2B", + "id": 48, + "mission": "Remote Sensing", + "weight": "694 kg (Mass at lift off)", + "onboard_orbit": "930 Watts", + "stabilization": "3 \u2013 axis body stabilised based on inputs from star sensors and gyros using Reaction wheels, Magnetic Torquers and Hydrazine Thrusters", + "payloads": "Panchromatic Camera", + "launch_date": "July 12, 2010", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C15", + "orbit": "630 kms, Polar Sun Synchronous", + "inclination": "97.71\u00ba" + }, + { + "name": "Oceansat-2", + "id": 47, + "date": "Sept 23, 2009", + "launch_site": "SHAR, Sriharikota", + "launch_vehicle": "PSLV - C14", + "orbit": "Polar Sun Synchronous", + "altitude": "720 km", + "inclination": "98.28\u00b0", + "period": "99.31 minutes", + "local_time_of_eq._crossing": "12 noon \u00b1 10 minutes", + "repetitivity_cycle": "2 days", + "payloads": "OCM, SCAT and ROSA", + "mass_at_lift_off": "960 kg", + "power": "15 Sq.m Solar panels generating 1360W, Two 24 Ah Ni-Cd Batteries", + "mission_life": "5 years" + }, + { + "name": "RISAT-2", + "id": 46, + "altitude": "550 km", + "inclination": "41 deg", + "orbit_period": "90 minutes", + "mass": "300 kg" + }, + { + "name": "Chandrayaan-1 ", + "id": 45, + "mission": "Remote Sensing, Planetary Science", + "weight": "1380 kg (Mass at lift off)", + "onboard_power": "700 Watts", + "stabilization": "3 - axis stabilised using reaction wheel and attitude control thrusters, sun sensors, star sensors, fibre optic gyros and accelerometers for attitude determination.", + "launch_date": "22 October 2008", + "launch_site": "SDSC, SHAR, Sriharikota", + "launch_vehicle": "PSLV - C11", + "orbit": "100 km x 100 km : Lunar Orbit", + "mission_life": "2 years" + }, + { + "name": "IMS-1", + "id": 44, + "orbit": "Polar Sun Synchronous", + "altitude": "635 km", + "mission_life": "2 years", + "physical_dimensions": "0.604x0.980x1.129 m", + "mass": "83 kg", + "power": "Two deployable sun pointing solar panels generating 220 W power, 105 Ah Lithium ion battery", + "telemetry,_tracking_and_command": "S-band", + "attitude_and_orbit_control_system": "Star Sensor, Miniature Sun Sensors, Magnetometers Gyros, Miniature Micro Reaction Wheels, Magnetic Torquers, single 1 N Hydrazine Thruster", + "data_handling": "S-band", + "data_storage": "16 Gb Solid State Recorder" + }, + { + "name": "CARTOSAT \u2013\n2A", + "id": 43, + "mission": "Remote Sensing", + "weight": "690 Kg (Mass at lift off)", + "onboard_power": "900 Watts", + "stabilization": "3 \u2013 axis body stabilised using high torque reaction wheels, magnetic torquers and hydrogen thrusters", + "payloads": "Panchromatic Camera", + "launch_date": "28 April 2008", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C9", + "orbit": "635 km, Polar Sun Synchronous", + "inclination": "97.94 deg", + "mission_life": "5 years" + }, + { + "name": "INSAT-4CR", + "id": 42, + "mission": "Communication", + "weight": "2,130 kg (Mass at Lift \u2013 off)", + "onboard_power": "3000 W", + "communication_payload": "12 Ku-band transponders employing 140 W Traveling Wave Tube Amplifiers (TWTA) Ku-band Beacon", + "launch_date": "September 2, 2007", + "launch_site": "SHAR, Sriharikota, India", + "launch_vehicle": "GSLV-F04", + "orbit": "Geosynchronous (74\u00b0 E)", + "mission_life": "12 Years" + }, + { + "name": "INSAT-4B", + "id": 41, + "mission": "Communication", + "weight": "3025 kg (at Lift \u2013 off)", + "onboard_power": "5859 W", + "stabilization": "It uses 3 earth sensors, 2 digital sun sensors, 8 coarse analog sun sensors, 3 solar panel sun sensors and one sensor processing electronics. The wheels and wheel drive electronics were imported with indigenous wheel interface module to interface the wheel drive electronics and AOCE.", + "propulsion": "The propulsion system is employing 16 thrusters, 4 each located on east, west and AY sides and 2 each on north and south sides. There is one 440 N liquid apogee motor (using Mono Methyl Hydrazine (MMH) as fuel and oxides of Nitrogen (MON3 as oxidizer) and three pressurant tanks mounted on the LAM deck.", + "payload": "12 Ku band high power transponders covering Indian main land using 140W radiatively cooled TWTAs.", + "launch_date": "March 12, 2007", + "launch_site": "French Guiana", + "launch_vehicle": "Ariane5", + "orbit": "Geostationary (93.5o E Longitude)", + "mission_life": "12 Years" + }, + { + "name": "CARTOSAT-2", + "id": 40, + "mission": "Remote Sensing", + "weight": "650 Kg", + "onboard_orbit": "900 Watts", + "stabilization": "3 - axis body stabilised using high torque reaction wheels, magnetic torquers and thrusters", + "payloads": "Panchromatic Camera", + "launch_date": "10 January 2007", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C7", + "orbit": "Polar Sun Synchronous", + "mission_life": "5 years" + }, + { + "name": "INSAT-4A", + "id": 39, + "spacecraft_mass": "Lift off 3081 Kg Dry Mass 1386.55 Kg", + "orbit": "Geostationary ( 83o E)", + "power": "Solar Array to provide a power of 5922 W", + "battery": "Three 70 Ah Ni H2 Batteries for eclipse support of 4264 W", + "life": "12 Years", + "launch_date": "December 22, 2005", + "launch_vehicle": "ARIANE5-V169" + }, + { + "name": "CARTOSAT-1", + "id": 38, + "launch_date": "5 May 2005", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C6", + "orbit": "618 km Polar Sun Synchronous", + "payloads": "PAN FORE, PAN - AFT", + "orbit_period": "97 min", + "number_of_orbits_per_day": "14", + "local_time_of_equator_crossing": "10:30 am", + "repetivity": "126 days", + "revisit": "5 days", + "lift-off_mass": "1560 kg", + "attitude_and_orbit_control": "3-axis body stabillised using reaction wheels, Magnetic Torquers and Hydrazine Thrusters", + "electrical_power": "15 sqm Solar Array generating 1100w, Two 24 Ah Ni-Cd batteries", + "mission_life": "5 years" + }, + { + "name": "HAMSAT", + "id": 37, + "launch_date": "May 5, 2005", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV-C6", + "orbit": "Geo-synchronous, 633.355 km (average)", + "payloads": "2 Transponders" + }, + { + "name": "EDUSAT", + "id": 36, + "mission": "Education", + "spacecraft_mass": "1950.5 kg mass (at Lift - off) 819.4 kg (Dry mass)", + "onboard_power": "Total four solar panel of size 2.54 M x 1.525 M generating 2040 W (EOL), two 24 AH NiCd batteries for eclipse support", + "stabilization": "3 axis body stabilised in orbit using sensors, momentum and reaction wheels, magnetic torquers and eight 10 N & 22N reaction control thrusters.", + "propulsion": "440 N Liquid Apogee Motor with MON - 3 and MMH for orbit raising", + "payload": "Six upper extended C - band transpondersFive lower Ku band transponders with regional beam coverage One lower Ku band National beam transponder with Indian main land coverageKu beacon12 C band high power transponders with extended coverage, covering southeast and northwest region apart from Indian main land using 63 W LTWTAs", + "launch_date": "September 20, 2004", + "launch_site": "SHAR, Sriharikota, India", + "launch_vehicle": "GSLV-F01", + "orbit": "Geostationary (74oE longitude)", + "mission_life": "7 Years (minimum)" + }, + { + "name": "IRS-P6 / RESOURCESAT-1", + "id": 35, + "launch_date": "October 17, 2003", + "launch_site": "SHAR, Sriharikota", + "launch_vehicle": "PSLV-C5", + "payloads": "LISS-4, LISS-3, AWiFS-A, AWiFS-B", + "orbit": "Polar Sun Synchronous", + "orbit_height": "817 km", + "orbit_inclination": "98.7o", + "orbit_period": "101.35 min", + "number_of_orbits_per_day": "14", + "local_time_of_equator_crossing": "10:30 am", + "repetivity_(liss-3)": "24 days", + "revisit": "5 days", + "lift-off_mass": "1360 kg", + "attitude_and_orbit_control": "3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", + "power": "Solar Array generating 1250 W, Two 24 Ah Ni-Cd batteries", + "mission_life": "5 years" + }, + { + "name": "INSAT-3E", + "id": 34, + "mission": "Communication", + "spacecraft_mass": "2,775 kg (Mass at Lift-off) 1218 kg (Dry mass)", + "launch_date": "September 28, 2003", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane5-V162", + "orbit": "Geostationary Orbit" + }, + { + "name": "GSAT-2", + "id": 33, + "mission": "Communication", + "weight": "1800 kg", + "launch_date": "May 8, 2003", + "launch_site": "SHAR, Sriharikota, India", + "launch_vehicle": "GSLV\u2013D2", + "orbit": "Geostationary orbit (48oE longitude)" + }, + { + "name": "INSAT-3A", + "id": 32, + "mission": "Telecommunication, broadcasting and Meteorology", + "spacecraft_mass": "2,950 kg (Mass at Lift\u2013off) 1,348 kg (Dry mass)", + "onboard_power": "3,100 W", + "stabilization": "3 \u2013 axis body stabilised in orbit using momentum and reaction wheels, solar flaps, magnetic torquers and eight 10 N and eight 22 N reaction control thrusters", + "propulsion": "440 N Liquid Apogee Motor with MON-3 (Mixed Oxides of Nitrogen) and MMH (Mono Methyl Hydrazine) for orbit raising", + "payload": "Communication payload- 12 C \u2013 band transponders, - 6 upper extended C band transponders - 6 Ku band transponders - 1 Satellite Aided Search & Rescue transponders Meteorological payload- Very High Resolution Radiometer (VHRR) with 2 km resolution in visible band and 8 km resolution in infrared and water vapour band- Charged Coupled Device (CCD) camera operating in visible, near infrared and shortwave infrared band with 1 km resolution.- Data Relay Transponders (DRT)", + "launch_date": "April 10, 2003", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane5-V160", + "orbit": "Geostationary (93.5o E longitude)", + "mission_life": "12 Years" + }, + { + "name": "KALPANA-1", + "id": 31, + "mission": "7 Years", + "spacecraft_mass": "1060 kg mass (at Lift \u2013 off) 498 kg (Dry mass)", + "onboard_power": "550 W", + "payload": "Very High Resolution Radiometer (VHRR) Data Relay Transponder (DRT)", + "launch_date": "12 September 2002", + "launch_site": "SHAR, Sriharikota", + "launch_vehicle": "PSLV \u2013 C4", + "orbit": "Geostationary (74 deg East longitude)" + }, + { + "name": "INSAT-3C", + "id": 30, + "mission": "Communication, broadcasting and Meteorology", + "spacecraft_mass": "2,650 kg (Mass at Lift - off) 1218 kg (Dry mass)", + "onboard_power": "2765 W", + "propulsion": "Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.", + "payload": "24 C band transponders 6 Extended C - band Transponders 2 S - band Transponders", + "launch_date": "January 24, 2002", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane5-V147", + "orbit": "Geostationary (74o longitude)", + "mission_life": "Very long" + }, + { + "name": "The Technology Experiment Satellite\n(TES)", + "id": 29, + "launch_date": "22 October 2001", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C3", + "orbit": "572 km Sun Synchronous", + "payloads": "PAN" + }, + { + "name": "PSLV-C3 / TES", + "id": 28, + "launch_date": "22 October 2001", + "launch_site": "SHAR Centre Sriharikota India", + "launch_vehicle": "PSLV- C3", + "orbit": "572 km Sun Synchronous", + "payloads": "PAN" + }, + { + "name": "GSAT-1", + "id": 27, + "mission": "Communication", + "weight": "1530 kg", + "launch_date": "18 April 2001", + "launch_site": "SHAR, Sriharikota", + "launch_vehicle": "GSLV \u2013 D1", + "orbit": "Sun Synchronous Geo stationary orbit" + }, + { + "name": "INSAT-3B", + "id": 26, + "mission": "Very long", + "spacecraft_mass": "2,070 (Mass at Lift \u2013 off) 970 kg (Dry mass)", + "onboard_power": "1,712 W", + "stabilization": "3 \u2013 axis body stabilised biased momentum control system using earth sensors, sun sensors, inertial reference unit, momentum / reaction wheels, magnetic torquers and unified bi-propellant thrusters.", + "propulsion": "Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.", + "payload": "12 extended C \u2013 band Transponders Five Ku band Transponders Mobile Satellite Services (MSS)", + "launch_date": "22nd March 2000", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane -5", + "orbit": "Geostationary (83 deg East longitude)", + "inclination": "7 deg" + }, + { + "name": "Oceansat(IRS-P4)", + "id": 25, + "launch_date": "May 26, 1999", + "launch_site": "SHAR, Sriharikota", + "launch_vehicle": "PSLV - C2", + "orbit": "Polar Sun Synchronous", + "altitude": "720 km", + "inclination": "98.28 deg", + "period": "99.31 min", + "local_time_of_eq._crossing": "12 noon", + "repetitivity_cycle": "2 days", + "size": "2.8m x 1.98m x 2.57m", + "mass_at_lift_off": "1050 kg", + "length_when_fully_deployed": "11.67 m", + "attitude_and_orbit_control": "3-axis body-stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters", + "power": "9.6 Sq.m Solar Array generating 750w Two 21 Ah Ni-Cd Batteries", + "mission_completed_on": "August 8, 2010" + }, + { + "name": "INSAT-2E", + "id": 24, + "mission": "Communication and Meteorology", + "spacecraft_mass": "2,550 kg (Mass at Lift-off) 1150 kg (Dry mass)", + "launch_date": "03 April 1999", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane \u2013 42P", + "orbit": "Geosynchronous (83 deg east longitude)" + }, + { + "name": "IRS-1D", + "id": 23, + "mission": "Operational Remote Sensing", + "weight": "1250 kg", + "onboard_power": "809 Watts (generated by 9.6 sq.metres Solar Panels)", + "communication": "S-band, X-band", + "stabilization": "Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer", + "rcs": "Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters", + "payload": "Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)", + "onboard_tape_recorder": "Storage Capacity : 62 G bits", + "launch_date": "December 28, 1995", + "launch_site": "Baikanur Cosmodrome Kazakhstan", + "launch_vehicle": "Molniya", + "orbit": "817 km Polar Sun-synchronous", + "inclination": "98.69o", + "repetivity": "24 days", + "local_time": "10.30 a.m", + "mission_completed_on": "September 21, 2007" + }, + { + "name": "INSAT-2D", + "id": 22, + "mission": "Communication", + "weight": "2079 kg with propellants, 995 kg dry weight", + "onboard_power": "1650 Watts", + "communication": "C, extended C, S and Ku bands", + "stabilization": "Three axis stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", + "propulsion": "Integrated bipropellan stystem ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.", + "payload": "Transponders: 16C-band / extended C-band transponders (forFSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders", + "launch_date": "June 4, 1997", + "launch_site": "French Guyana", + "launch_vehicle": "Arianev 4", + "orbit": "Geostationary 93,.5deg.E", + "inclination": "0 deg." + }, + { + "name": "IRS-P3", + "id": 21, + "mission": "Remote sensing of earth's natural resources. Study of X-ray Astronomy. Periodic calibration of PSLV tracking radar located at tracking stations.", + "weight": "920 kg", + "onboard_power": "817 Watts", + "communication": "S-band", + "stabilization": "Three axis body stabilized", + "rcs": "Combinations of bladder type and surface tension type mass expulsion monopropellant hydrazine system", + "payload": "WideField Sensor (WiFS), Modular Opto - electronic Scanner (MOS), Indian X-ray Astronomy Experiment (IXAE), C-band transponder(CBT)", + "launch_date": "March 21, 1996", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV-D3", + "orbit": "817 km. Circular polar sun-synchronous with equatorial crossing at 10.30 am (descending node)", + "inclination": "98.68o", + "repetivity": "WiFS : 5 days", + "mission_completed_during": "January 2006" + }, + { + "name": "IRS-1C", + "id": 20, + "mission": "Operational Remote Sensing", + "weight": "1250 kg", + "onboard_power": "809 Watts (generated by 9.6 sq.metres Solar Panels)", + "communication": "S-band, X-band", + "stabilization": "Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer", + "rcs": "Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters", + "payload": "Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)", + "onboard_tape_recorder": "Storage Capacity : 62 G bits", + "launch_date": "December 28, 1995", + "launch_site": "Baikanur Cosmodrome Kazakhstan", + "launch_vehicle": "Molniya", + "orbit": "817 km Polar Sun-synchronous", + "inclination": "98.69o", + "repetivity": "24 days", + "local_time": "10.30 a.m", + "mission_completed_on": "September 21, 2007" + }, + { + "name": "INSAT-2C", + "id": 19, + "mission": "Communication", + "weight": "2106 kg with propellants 946 kg dry weight", + "onboard_power": "1320 Watts", + "communication": "C extended C, S and Ku bands", + "stabilization": "Three axis stabilized with two Momen'tum Wheels & one Reaction Wheel, Magnetic torquers", + "propulsion": "Integrated bipropellant system ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.", + "payload": "Transponders: 16C-band / extended C-band transponders (for FSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders", + "launch_date": "December 7, 1995", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane4", + "orbit": "Geostationary 93.5 deg E", + "inclination": "0 deg.", + "mission_life": "Seven years(nominal)", + "orbit_life": "Very Long" + }, + { + "name": "IRS-P2", + "id": 18, + "mission": "Operational Remote Sensing", + "weight": "804 kg", + "onboard_power": "510 Watts", + "communication": "S-band, X-band", + "stabilization": "Three axis body stabilized with 4 Reaction Wheels, Magnetic torquers", + "rcs": "4 tanks containing Monopropellant Hydrazine based with sixteen 1 N thrusters and one 11 N thruster", + "payload": "Two solid state Push Broom Cameras operating in four spectral bands in the visible and near-IR range using CCD arrays: LlSS-2A & LlSS-2B (Resolution: 32.74 metre)", + "launch_date": "October 15, 1994", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV-D2", + "inclination": "98.68o", + "repetivity": "24 days", + "mission_completed_on": "1997" + }, + { + "name": "SROSS-C2", + "id": 17, + "mission": "Experimental", + "weight": "115 kg", + "onboard_power": "45 Watts", + "communication": "S-band and VHF", + "rcs": "Monopropellant Hydrazine based with six 1 Newton thrusters", + "payload": "Gamma Ray Burst (GRB) & Retarding Potential Analyser (RPA)", + "launch_date": "May 04,1994", + "launch_site": "SHAR Centre,Sriharikota,India", + "launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", + "orbit": "430 x 600 km.", + "inclination": "45 deg.", + "mission_life": "Six months (nominal)", + "orbital_life": "Two years (nominal)" + }, + { + "name": "IRS-1E", + "id": 16, + "mission": "Operational Remote Sensing", + "weight": "846 kg", + "onboard_power": "415 Watts", + "communication": "S-band (TIC) & VHF", + "stabilization": "Three axis body stabilized ( zero momentum) with 4 Reaction Wheels, Magnetic torquers", + "rcs": "Monopropellant Hydrazine based RCS with 1 Newton thrusters ( 16 Nos.)", + "payload": "LlSS-1 MEOSS (Mono-ocula Erlectro Optic Stereo Scanner)", + "launch_date": "September 20, 1993", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "PSLV-D1", + "orbit": "Not realised" + }, + { + "name": "INSAT-2B", + "id": 15, + "mission": "Multipurpose Communication, meteorology and Satellite based search and rescue", + "weight": "1906 kg with propellant 916 kg dry weight", + "onboard_power": "One KW approx.", + "communication": "C, extended C and S band", + "stabilization": "Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", + "propulsion": "Integrated bipropellant system ( MMH and N2 04) With sixteen 22 N thrusters and 440 N LAM.", + "payload": "Transponders: 12C-band (for FSS),6 ext. C-band (for FSS) 2S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band", + "launch_date": "July 23, 1993", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane 4", + "orbit": "Geostationary 93.5o E", + "inclination": "0o", + "mission_life": "Seven years(nominal)", + "orbit_life": "Very Long" + }, + { + "name": "INSAT-2A", + "id": 14, + "mission": "Multipurpose Communication, meteorology and Satellite based search and rescue", + "weight": "1906 kg with propellant 916 kg dry weight", + "onboard_power": "One KW approx", + "communication": "C, extended C and S band", + "stabilization": "Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers", + "propulsion": "Integrated bipropellant system (MMH and N2 04) With sixteen 22 N thrusters and 440 LAM.", + "payload": "Transponders: 12 C-band (for FSS),6 ext. C-band (for FSS) 2 S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band", + "launch_date": "July 10,1992", + "launch_site": "French Guyana", + "launch_vehicle": "Ariane 4", + "orbit": "Geostationary 74oE longitude", + "inclination": "0o", + "mission_life": "Seven years(nominal)", + "orbit_life": "Very Long" + }, + { + "name": "SROSS-C\n", + "id": 13, + "mission": "Experimental", + "weight": "106.1 kg", + "onboard_power": "45 Watts", + "communication": "S-band and VHF", + "stabilization": "Spin stabilized with a Magnetic Torquer and Magnetic Bias Control", + "payload": "Gamma Ray Burst (GRB) experiment & Retarding Potential Analyser (RPA) experiment", + "launch_date": "May 20,1992", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", + "orbit": "267 x 391 km", + "mission_life": "Two months (Re-entered on July15,1992)" + }, + { + "name": "IRS-1B", + "id": 12, + "mission": "Operational Remote Sensing", + "weight": "975 kg", + "onboard_power": "600 Watts", + "communication": "S-band, X-band and VHF (commanding only)", + "stabilization": "Three axis body stabilized (zero momentum) with 4 Reactions Wheels, Magnetic torquers", + "rcs": "Monopropellant Hydrazine based with sixteen 1 Newton thrusters", + "payload": "Three solid state Push Broom Cameras LlSS-1 (72.5 metre resolution), LlSS-2A and LlSS-2B (36.25 metre resolution)", + "launch_date": "August 29, 1991", + "launch_site": "Baikanur Cosmodrome Kazakhstan", + "launch_vehicle": "Vostok", + "orbit": "904 km Polar Sun Synchronous", + "inclination": "99.08o", + "repetivity": "22 days", + "local_time": "10.30 a.m. (descending node)", + "mission_completed_on": "December 20, 2003" + }, + { + "name": "SROSS-2", + "id": 11, + "mission": "Experimental", + "weight": "150 kg", + "onboard_power": "90 Watts", + "communication": "S-band and VHF", + "stabilization": "Three axis body stabilized (biased momentum) with a MomentumWheel and Magnetic Torquer", + "propulsion_system": "Monopropellant (Hydrazine based) Reaction Control System", + "payload": "Gamma Ray Burst (GRB) payload and Mono PayloadOcular Electro-Optic Stereo Scanner (MEOSS) built by DLR, Germany", + "launch_date": "July 13, 1988", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", + "orbit": "Not realised" + }, + { + "name": "IRS-1A", + "id": 10, + "mission": "Operational Remote Sensing", + "weight": "975 kg", + "onboard_power": "600 Watts", + "communication": "S-band, X-band and VHF(commanding only)", + "stabilization": "Three axis body stabilized (zero momentum)with 4 Reactions Wheels, Magnetic torquers", + "rcs": "Monopropellant Hydrazine based with sixteen 1 Newton thrusters", + "payload": "Three solid state Push Broom Cameras: LISS-1(72.5 metre resolution),LISS-2A and LISS-2B (36.25 metre resolution)", + "launch_date": "March 17, 1988", + "launch_site": "Baikanur Cosmodrome Kazakhstan", + "launch_vehicle": "Vostok", + "orbit": "904 km Polar Sun-synchronous", + "inclination": "99.08o", + "repetivity": "22 days (307 orbits)", + "local_time": "10.30 a.m. (descending node)", + "mission_completed_during": "July 1996" + }, + { + "name": "SROSS-1\n", + "id": 9, + "mission": "Experimental", + "weight": "150 kg", + "onboard_power": "90 Watts", + "communication": "S-band and VHF", + "stabilization": "Three axis body stabilized (biased momentum) with a Momentum Wheel and Magnetic Torquer", + "propulsion_system": "Monopropellant (Hydrazine based) Reaction control system", + "payload": "Launch Vehicle Monitoring Platform(LVMP), Gamma Ray Burst (GRB) payload and Corner Cube Retro Reflector (CCRR) for laser tracking", + "launch_date": "March 24, 1987", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "Augmented Satellite Launch Vehicle (ASLV)", + "orbital_life": "Not realised" + }, + { + "name": "Rohini Satellite RS-D2", + "id": 8, + "mission": "Experimental", + "weight": "41.5 kg", + "onboard_power": "16 Watts", + "communication": "VHF band", + "stabilization": "Spin stabilized", + "payload": "Smart sensor (remote sensing payload),L-band beacon", + "launch_date": "April 17, 1983", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "SLV-3", + "orbit": "371 x 861 km", + "inclination": "46o", + "mission_life": "17 months", + "orbital_life": "Seven years (Re-entered on April 19, 1990)" + }, + { + "name": "Bhaskara-II", + "id": 7, + "mission": "Experimental Remote Sensing", + "weight": "444 kg", + "onboard_power": "47 Watts", + "communication": "VHF band", + "stabilization": "Spin stabilized (spin axis controlled)", + "payload": "TV cameras, three band Microwave Radiometer (SAMIR)", + "launch_date": "Nov 20, 1981", + "launch_site": "Volgograd Launch Station (presently in Russia)", + "launch_vehicle": "C-1 Intercosmos", + "orbit": "541 x 557 km", + "inclination": "50.7o", + "mission_life": "One year (nominal)", + "orbital_life": "About 10 years ( Re-entered in 1991 )" + }, + { + "name": "APPLE", + "id": 6, + "mission": "Experimental geostationary communication", + "weight": "670 kg", + "onboard_power": "210 Watts", + "communication": "VHF and C-band", + "stabilization": "Three axis stabilized (biased momentum) with Momentum Wheels, Torquers & Hydrazine based Reaction control system", + "payload": "C - band transponders (Two)", + "launch_date": "June19,1981", + "launch_site": "Kourou (CSG), French Guyana", + "launch_vehicle": "Ariane -1(V-3)", + "orbit": "Geosynchronous (102 deg. E longitude, over Indonesia)", + "inclination": "Near zero", + "mission_life": "Two years" + }, + { + "name": "Rohini Satellite RS-D1", + "id": 5, + "mission": "Experimental", + "weight": "38 kg", + "onboard_power": "16 Watts", + "communication": "VHF band", + "stabilization": "Spin stabilized", + "payload": "Landmark Tracker ( remote sensing payload)", + "launch_date": "May 31,1981", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "SLV-3", + "orbit": "186 x 418 km (achieved)", + "inclination": "46 deg", + "orbital_life": "Nine days" + }, + { + "name": "Rohini Satellite RS-1", + "id": 4, + "mission": "Experimental", + "weight": "35 kg", + "onboard_power": "16 Watts", + "communication": "VHF band", + "stabilization": "Spin stabilized", + "payload": "Launch vehicle monitoring instruments", + "launch_date": "July 18,1980", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "SLV-3", + "orbit": "305 x 919 km", + "inclination": "44.7 deg.", + "mission_life": "1.2 years", + "orbital_life": "20 months" + }, + { + "name": "Rohini Technology Payload (RTP)", + "id": 3, + "mission": "Experimental", + "weight": "35 kg", + "onboard_power": "3 Watts", + "communication": "VHF band", + "stabilization": "Spin stabilized (spin axis controlled)", + "payload": "Launch vehicle monitoring instruments", + "launch_date": "August 10,1979", + "launch_site": "SHAR Centre, Sriharikota, India", + "launch_vehicle": "SLV-3", + "orbit": "Not achieved" + }, + { + "name": "Bhaskara-I", + "id": 2, + "mission": "Experimental Remote Sensing", + "weight": "442 kg", + "onboard_power": "47 Watts", + "communication": "VHF band", + "stabilization": "Spin stabilized (spin axis controlled)", + "payload": "TVcameras, three band Microwave Radiometer (SAMIR)", + "launch_date": "Jun 07,1979", + "launch_site": "Volgograd Launch Station (presently in Russia)", + "launch_vehicle": "C-1Intercosmos", + "orbit": "519 x 541 km", + "inclination": "50.6 deg", + "mission_life": "One year (nominal)", + "orbital_life": "About 10 years ( Re-entered in 1989 )" + }, + { + "name": "Aryabhata ", + "id": 1, + "mission": "Scientific/ Experimental", + "weight": "360 kg", + "on_board_power": "46 Watts", + "communication": "VHF band", + "stabilization": "Spinstabilize", + "payload": "X-ray Astronomy Aeronomy & Solar Physics", + "launch_date": "April 19, 1975", + "launch_site": "Volgograd Launch Station (presently in Russia)", + "launch_vehicle": "C-1 Intercosmos", + "orbit": "563 x 619 km", + "inclination": "50.7 deg", + "mission_life": "6 months(nominal), Spacecraft mainframe active till March,1981", + "orbital_life": "Nearly seventeen years (Re-entered on February 10,1992)" + } ] From 018cbbb0a0e49250d5ba30ad07a250ca0a4188af Mon Sep 17 00:00:00 2001 From: Anin Arafath Date: Sat, 15 Apr 2023 22:00:40 +0530 Subject: [PATCH 9/9] =?UTF-8?q?jupiter=20script=20for=20scraping=20space?= =?UTF-8?q?=20mission=20data=20of=20isro=20=F0=9F=9A=80?= MIME-Version: 1.0 Content-Type: text/plain; charset=UTF-8 Content-Transfer-Encoding: 8bit --- isro_scrape/scraping.ipynb | 1084 ++++++++++++++++++++++++++++++++++++ 1 file changed, 1084 insertions(+) create mode 100644 isro_scrape/scraping.ipynb diff --git a/isro_scrape/scraping.ipynb b/isro_scrape/scraping.ipynb new file mode 100644 index 0000000..f82c177 --- /dev/null +++ b/isro_scrape/scraping.ipynb @@ -0,0 +1,1084 @@ +{ + "cells": [ + { + "cell_type": "code", + "execution_count": 221, + "metadata": {}, + "outputs": [], + "source": [ + "#essential packages \n", + "import requests\n", + "from bs4 import BeautifulSoup\n", + "import json" + ] + }, + { + "cell_type": "code", + "execution_count": 222, + "metadata": {}, + "outputs": [], + "source": [ + "# URL of the file containing the results of the analysis\n", + "# access the web content \n", + "URL = \"https://www.isro.gov.in/SpacecraftMissions.html#\"\n", + "response = requests.get(URL)\n" + ] + }, + { + "cell_type": "code", + "execution_count": 223, + "metadata": {}, + "outputs": [], + "source": [ + "soup = BeautifulSoup(response.text,'lxml')\n", + "spacecrafts = soup.find_all(\"a\", {\"class\":\"out\"})\n" + ] + }, + { + "cell_type": "code", + "execution_count": 232, + "metadata": {}, + "outputs": [ + { + "name": "stdout", + "output_type": "stream", + "text": [ + "[\n", + " {\n", + " \"name\": \"RISAT-2BR1\",\n", + " \"id\": 1,\n", + " \"lift-off_weight\": \"628 kg\",\n", + " \"altitude\": \"576 km\",\n", + " \"payload\": \"X-Band Radar\",\n", + " \"inclination\": \"37 deg\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"Cartosat-3\",\n", + " \"id\": 1,\n", + " \"mean________________________________________________________________altitude\": \"509 km\",\n", + " \"mean_inclination\": \"97.5\\u00b0\",\n", + " \"overall_mass\": \"1625 kg\",\n", + " \"power_generation\": \"2000W\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-15\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication and Satellite Navigation\",\n", + " \"weight\": \"3164 kg (Mass at Lift \\u2013 off) 1440 kg (Dry Mass)\",\n", + " \"power\": \"Solar array providing 6200 Watts and Three 100 AH Lithium-Ion batteries\",\n", + " \"propulsion\": \"Bi- propellant System\",\n", + " \"launch____________________________________________________________date\": \"November 11, 2015\",\n", + " \"launch____________________________________________________________site\": \"Kourou, French Guiana\",\n", + " \"launch____________________________________________________________vehicle\": \"Ariane-5 VA-227\",\n", + " \"orbit\": \"Geostationary (93.5\\u00b0 East longitude) Co-located with INSAT-3A and INSAT-4B\",\n", + " \"mission____________________________________________________________life\": \"12 Years\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-6\",\n", + " \"id\": 1,\n", + " \"physical____________________________________________________________properties\": \"Lift off Mass : 2117 kg Main Structure : I-2K Overall size(m) : 2.1 x 2.5 x 4.1\",\n", + " \"power\": \"Generated power 3100 W\",\n", + " \"aocs\": \"Momentum biased 3-axis stabilised\",\n", + " \"antennas\": \"One 0.8 m (fixed) and one 6 m unfurlable antenna (transmit and receive)\",\n", + " \"communication____________________________________________________________payloads\": \"i. S-band payload with five spot beams covering India for user links ii. C-band payload with one beam covering India for hub links S-band payload uses 6 m unfurlable antenna and C-band uses 0.8 m antenna.\",\n", + " \"mission_life\": \"9 years\"\n", + " },\n", + " {\n", + " \"name\": \"IRNSS-1B\",\n", + " \"id\": 1,\n", + " \"off_mass\": \"1432 kg\",\n", + " \"physical_dimensions\": \"1.58 metre x 1.50 metre x 1.50 metre\",\n", + " \"orbit\": \"Geosynchronous, at 55 deg East longitude with 29 deg inclination\",\n", + " \"power\": \"Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity\",\n", + " \"propulsion\": \"440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters\",\n", + " \"control_system\": \"Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators\",\n", + " \"mission_life\": \"10 years\",\n", + " \"launch_date\": \"Apr 04, 2014\",\n", + " \"launch_site\": \"SDSC SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV - C24\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-14\",\n", + " \"id\": 1,\n", + " \"mass_at_lift-off\": \"1982 kg\",\n", + " \"overall_size_(m)\": \"2.0 X 2.0 X 3.6\",\n", + " \"power\": \"2600 W\",\n", + " \"attitude_and_orbit_control_system_(aocs)\": \"Momentum biased 3-axis stabilized mode\",\n", + " \"propulsion_system\": \"Bi propellant-Mono Methyl Hydrazine and Mixed Oxides of Nitrogen (MON-3)\",\n", + " \"antennae\": \"One 2m and one 2.2 m single shell shaped reflector Antennae (transmit and receive)\",\n", + " \"launch_date\": \"January 05, 2014\",\n", + " \"launch_site\": \"SDSC, SHAR\",\n", + " \"launch_vehicle\": \"GSLV-D5\",\n", + " \"orbit\": \"74 deg East longitude in geostationary orbit\",\n", + " \"mission_life\": \"12 Years\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-7\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"mass_at_lift-off\": \"2650 kg\",\n", + " \"physical_dimensions\": \"3.1 m X 1.7 m X 2.0 m\",\n", + " \"power\": \"3,000 W (end of life)\",\n", + " \"satbilisation\": \"3-axis stabilized\",\n", + " \"launch_date\": \"August 30, 2013\",\n", + " \"launch_site\": \"Kourou, French Guiana\",\n", + " \"launch_vehicle\": \"Ariane-5 VA-215\",\n", + " \"orbit\": \"74oE Geo Stationary\",\n", + " \"mission_life\": \"> 7 Years\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-3D\",\n", + " \"id\": 1,\n", + " \"mission\": \"Meteorological and Search & Rescue Services\",\n", + " \"mass_at_lift-off\": \"2060 kg\",\n", + " \"power\": \"Solar panel generating 1164 W Two 18 Ah Ni-Cd batteries\",\n", + " \"physical_dimensions\": \"2.4m x 1.6m x 1.5m\",\n", + " \"propulsion\": \"440 Newton Liquid Apogee Motor (LAM) and twelve 22 Newton thrusters with Mono Methyl Hydrazine (MMH) as fuel and mixed Oxides of Nitrogen (MON-3) as oxidizer\",\n", + " \"stabilisation\": \"3-asix body stabilized in orbit using Sun Sensors, Star Sensors, gyroscopes, Momentum and Reaction Wheels, Magnetic Torquers and thrusters\",\n", + " \"antennae\": \"0.9m and 1.0m body mounted antennas\",\n", + " \"launch_date\": \"July 26, 2013\",\n", + " \"launch_site\": \"Kourou, French Guiana\",\n", + " \"launch_vehicle\": \"Ariane-5 VA-214\",\n", + " \"orbit\": \"Geostationary, 82 deg E Longitude\",\n", + " \"mission_life\": \"7 Years\"\n", + " },\n", + " {\n", + " \"name\": \"IRNSS-1A\",\n", + " \"id\": 1,\n", + " \"lift-off_mass\": \"1425 kg\",\n", + " \"physical_dimensions\": \"1.58 metre x 1.50 metre x 1.50 metre\",\n", + " \"orbit\": \"Geosynchronous, at 55 deg East longitude with 29 deg inclination\",\n", + " \"power\": \"Two solar panels generating 1660 W, one lithium-ion battery of 90 Ampere-Hour capacity\",\n", + " \"propulsion\": \"440 Newton Liquid Apogee Motor, twelve 22 Newton Thrusters\",\n", + " \"control_system\": \"Zero momentum system, orientation input from Sun & star Sensors and Gyroscopes; Reaction Wheels, Magnetic Torquers and 22 Newton thrusters as actuators\",\n", + " \"mission_life\": \"10 years\",\n", + " \"launch_date\": \"Jul 01, 2013\",\n", + " \"launch_site\": \"SDSC SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV - C22\"\n", + " },\n", + " {\n", + " \"name\": \"SARAL\",\n", + " \"id\": 1,\n", + " \"lift-off_mass\": \"407 kg\",\n", + " \"orbit\": \"781 km polar Sun synchronous\",\n", + " \"sensors\": \"4 PI sun sensors, magnetometer, star sensors and miniaturised gyro based Inertial Reference Unit\",\n", + " \"orbit_inclination\": \"98.538o\",\n", + " \"local_time_of_equator\": \"18:00 hours crossing\",\n", + " \"power\": \"Solar Array generating 906 W and 46.8 Ampere-hour Lithium-ion battery\",\n", + " \"onboard_data_storage\": \"32 Gb\",\n", + " \"attitude_and_orbit_control\": \"3-axis stabilisation with reaction wheels, Hydrazine Control System based thrusters\",\n", + " \"mission_life\": \"5 years\",\n", + " \"launch_date\": \"Feb 25, 2013\",\n", + " \"launch_site\": \"SDSC SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV - C20\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-10\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"3400 kg (Mass at Lift \\u2013 off) 1498 kg (Dry Mass)\",\n", + " \"power\": \"Solar array providing 6474 Watts (at Equinox) and two 128 AH Lithium-Ion batteries\",\n", + " \"physical_dimensions\": \"2.0 m X 1.77 m X 3.1 m cuboid\",\n", + " \"propulsion\": \"440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.\",\n", + " \"stabilisation\": \"3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters\",\n", + " \"antennae\": \"East : 2.2 m dia circular deployable Dual Gridded Reflector (DGR) West : 2.2 m X 2.4 m elliptical deployable DGR Earth Viewing Face (top) : 0.7 m parabolic, 0.9 m parabolic and 0.8 m X 0.8 m sixteen element helical antenna for GAGAN\",\n", + " \"launch_date\": \"September 29, 2012\",\n", + " \"launch_site\": \"Kourou, French Guiana\",\n", + " \"launch_vehicle\": \"Ariane-5 VA-209\",\n", + " \"orbit\": \"Geostationary (83\\u00b0 East longitude), co-located with INSAT-4A and GSAT-12\",\n", + " \"mission_life\": \"15 Years\"\n", + " },\n", + " {\n", + " \"name\": \"RISAT-1\",\n", + " \"id\": 1,\n", + " \"mass\": \"1858 kg\",\n", + " \"orbit\": \"Circular Polar Sun Synchronous\",\n", + " \"orbit_altitude\": \"536 km\",\n", + " \"orbit_inclination\": \"97.552o\",\n", + " \"orbit_period\": \"95.49 min\",\n", + " \"number_of_orbits_per_day\": \"14\",\n", + " \"local_time_of_equator_crossing\": \"6:00 am / 6:00 pm\",\n", + " \"power\": \"Solar Array generating 2200 W and one 70 AH Ni-H2 battery\",\n", + " \"repetivity\": \"25 days\",\n", + " \"attitude_and_orbit_control\": \"3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters\",\n", + " \"nominal_mission_life\": \"5 years\",\n", + " \"launch_date\": \"April 26, 2012\",\n", + " \"launch_site\": \"SDSC SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV- C19\"\n", + " },\n", + " {\n", + " \"name\": \"Megha-Tropiques\",\n", + " \"id\": 1,\n", + " \"lift-off_mass\": \"1000 kg\",\n", + " \"orbit\": \"867 km with an inclination of 20 deg to the equator\",\n", + " \"thermal\": \"Passive system with IRS heritage\",\n", + " \"power\": \"1325 W (at End of Life) Two 24 AH NiCd batteries\",\n", + " \"ttc\": \"S-band\",\n", + " \"attitude_and_orbit_control\": \"3-axis stabilised with 4 Reaction Wheels, Gyros and Star sensors, Hydrazine based RCS\",\n", + " \"solid_state_recorder\": \"16 Gb\",\n", + " \"launch_date\": \"October 12, 2011\",\n", + " \"launch_site\": \"SDSC SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV- C18\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-12\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"1410 kg (Mass at Lift \\u2013 off) 559 kg (Dry Mass)\",\n", + " \"power\": \"Solar array providing 1430 Watts and one 64 Ah Li-Ion batteries\",\n", + " \"physical_dimensions\": \"1.485 x 1.480 x 1.446 m cuboid\",\n", + " \"propulsion\": \"440 Newton Liquid Apogee Motors (LAM) with Mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.\",\n", + " \"attitude_orbit_control\": \"3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters\",\n", + " \"antennae\": \"One 0.7 m diameter body mounted parabolic receive antenna and one 1.2 m diameter polarisation sensitive deployable antenna\",\n", + " \"launch_date\": \"July 15, 2011\",\n", + " \"launch_site\": \"SHAR, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV-C17\",\n", + " \"orbit\": \"Geosynchronous (83\\u00b0 longitude)\",\n", + " \"mission_life\": \"About 8 Years\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-8\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"3093 kg (Mass at Lift \\u2013 off) 1426 kg (Dry Mass)\",\n", + " \"power\": \"Solar array providing 6242 watts three 100 Ah Lithium Ion batteries\",\n", + " \"physical_dimensions\": \"2.0 x 1.77 x 3.1m cuboid\",\n", + " \"propulsion\": \"440 Newton Liquid Apogee Motors (LAM) with mono Methyl Hydrazine (MMH) as fuel and Mixed oxides of Nitrogen (MON-3) as oxidizer for orbit raising.\",\n", + " \"stabilisation\": \"3-axis body stabilised in orbit using Earth Sensors, Sun Sensors, Momentum and Reaction Wheels, Magnetic Torquers and eight 10 Newton and eight 22 Newton bipropellant thrusters\",\n", + " \"antennas\": \"Two indigenously developed 2.2 m diameter transmit/receive polarisation sensitive dual grid shaped beam deployable reflectors with offset-fed feeds illumination for Ku-band; 0.6 m C-band and 0.8x0.8 sq m L-band helix antenna for GAGAN\",\n", + " \"launch_date\": \"May 21, 2011\",\n", + " \"launch_site\": \"Kourou, French Guiana\",\n", + " \"launch_vehicle\": \"Ariane-5 VA-202\",\n", + " \"orbit\": \"Geosynchronous (55\\u00b0 E)\",\n", + " \"mission_life\": \"More Than 12 Years\"\n", + " },\n", + " {\n", + " \"name\": \"RESOURCESAT-2\",\n", + " \"id\": 1,\n", + " \"mission\": \"Remote Sensing\",\n", + " \"orbit\": \"Circular Polar Sun Synchronous\",\n", + " \"orbit_altitude_at_injection\": \"822 km + 20 km (3 Sigma)\",\n", + " \"orbit_inclination\": \"98.731\\u00ba + 0.2\\u00ba\",\n", + " \"lift-off_mass\": \"1206 kg\",\n", + " \"orbit_period\": \"101.35 min\",\n", + " \"number_of_orbits_per_day\": \"14\",\n", + " \"local_time_of_equator_crossing\": \"10:30 am\",\n", + " \"repetivity\": \"24 days\",\n", + " \"attitude_and_orbit_control\": \"3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters\",\n", + " \"power\": \"Solar Array generating 1250 W at End Of Life, two 24 AH Ni-Cd batteries\",\n", + " \"launch_date\": \"April 20, 2011\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C16\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"YOUTHSAT\",\n", + " \"id\": 1,\n", + " \"lift-off_mass\": \"92 kg\",\n", + " \"orbit_period\": \"101.35 min\",\n", + " \"dimension\": \"1020 (Pitch) x 604 (Roll) x 1340 (Yaw) mm3\",\n", + " \"attitude_and_orbit_control\": \"3-axis body stabilised using Sun and Star Sensors, Miniature Magnetometer, Miniature Gyros, Micro Reaction Wheels and Magnetic Torquers\",\n", + " \"power\": \"Solar Array generating 230 W, one 10.5 AH Li-ion battery\",\n", + " \"mechanisms\": \"Paraffin Actuator based Solar Panel Hold Down and Release Mechanism\",\n", + " \"launch_date\": \"April 20, 2011\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C16\",\n", + " \"orbit\": \"Circular Polar Sun Synchronous\",\n", + " \"orbit_altitude_at_injection\": \"822 km\\u00a0+\\u00a020 km (3 Sigma)\",\n", + " \"orbit_inclination\": \"98.731 \\u00ba\\u00a0+\\u00a00.2 \\u00ba\",\n", + " \"mission_life\": \"2 years\"\n", + " },\n", + " {\n", + " \"name\": \"CARTOSAT-2B\",\n", + " \"id\": 1,\n", + " \"mission\": \"Remote Sensing\",\n", + " \"weight\": \"694 kg (Mass at lift off)\",\n", + " \"onboard_orbit\": \"930 Watts\",\n", + " \"stabilization\": \"3 \\u2013 axis body stabilised based on inputs from star sensors and gyros using Reaction wheels, Magnetic Torquers and Hydrazine Thrusters\",\n", + " \"payloads\": \"Panchromatic Camera\",\n", + " \"launch_date\": \"July 12, 2010\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C15\",\n", + " \"orbit\": \"630 kms, Polar Sun Synchronous\",\n", + " \"inclination\": \"97.71\\u00ba\"\n", + " },\n", + " {\n", + " \"name\": \"Oceansat-2\",\n", + " \"id\": 1,\n", + " \"date\": \"Sept 23, 2009\",\n", + " \"launch_site\": \"SHAR, Sriharikota\",\n", + " \"launch_vehicle\": \"PSLV - C14\",\n", + " \"orbit\": \"Polar Sun Synchronous\",\n", + " \"altitude\": \"720 km\",\n", + " \"inclination\": \"98.28\\u00b0\",\n", + " \"period\": \"99.31 minutes\",\n", + " \"local_time_of_eq._crossing\": \"12 noon \\u00b1 10 minutes\",\n", + " \"repetitivity_cycle\": \"2 days\",\n", + " \"payloads\": \"OCM, SCAT and ROSA\",\n", + " \"mass_at_lift_off\": \"960 kg\",\n", + " \"power\": \"15 Sq.m Solar panels generating 1360W, Two 24 Ah Ni-Cd Batteries\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"RISAT-2\",\n", + " \"id\": 1,\n", + " \"altitude\": \"550 km\",\n", + " \"inclination\": \"41 deg\",\n", + " \"orbit_period\": \"90 minutes\",\n", + " \"mass\": \"300 kg\"\n", + " },\n", + " {\n", + " \"name\": \"Chandrayaan-1 \",\n", + " \"id\": 1,\n", + " \"mission\": \"Remote Sensing, Planetary Science\",\n", + " \"weight\": \"1380 kg (Mass at lift off)\",\n", + " \"onboard_power\": \"700 Watts\",\n", + " \"stabilization\": \"3 - axis stabilised using reaction wheel and attitude control thrusters, sun sensors, star sensors, fibre optic gyros and accelerometers for attitude determination.\",\n", + " \"launch_date\": \"22 October 2008\",\n", + " \"launch_site\": \"SDSC, SHAR, Sriharikota\",\n", + " \"launch_vehicle\": \"PSLV - C11\",\n", + " \"orbit\": \"100 km x 100 km : Lunar Orbit\",\n", + " \"mission_life\": \"2 years\"\n", + " },\n", + " {\n", + " \"name\": \"IMS-1\",\n", + " \"id\": 1,\n", + " \"orbit\": \"Polar Sun Synchronous\",\n", + " \"altitude\": \"635 km\",\n", + " \"mission_life\": \"2 years\",\n", + " \"physical_dimensions\": \"0.604x0.980x1.129 m\",\n", + " \"mass\": \"83 kg\",\n", + " \"power\": \"Two deployable sun pointing solar panels generating 220 W power, 105 Ah Lithium ion battery\",\n", + " \"telemetry,_tracking_and_command\": \"S-band\",\n", + " \"attitude_and_orbit_control_system\": \"Star Sensor, Miniature Sun Sensors, Magnetometers Gyros, Miniature Micro Reaction Wheels, Magnetic Torquers, single 1 N Hydrazine Thruster\",\n", + " \"data_handling\": \"S-band\",\n", + " \"data_storage\": \"16 Gb Solid State Recorder\"\n", + " },\n", + " {\n", + " \"name\": \"CARTOSAT \\u2013\\n 2A\",\n", + " \"id\": 1,\n", + " \"mission\": \"Remote Sensing\",\n", + " \"weight\": \"690 Kg (Mass at lift off)\",\n", + " \"onboard_power\": \"900 Watts\",\n", + " \"stabilization\": \"3 \\u2013 axis body stabilised using high torque reaction wheels, magnetic torquers and hydrogen thrusters\",\n", + " \"payloads\": \"Panchromatic Camera\",\n", + " \"launch_date\": \"28 April 2008\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C9\",\n", + " \"orbit\": \"635 km, Polar Sun Synchronous\",\n", + " \"inclination\": \"97.94 deg\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-4CR\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"2,130 kg (Mass at Lift \\u2013 off)\",\n", + " \"onboard_power\": \"3000 W\",\n", + " \"communication_payload\": \"12 Ku-band transponders employing 140 W Traveling Wave Tube Amplifiers (TWTA) Ku-band Beacon\",\n", + " \"launch_date\": \"September 2, 2007\",\n", + " \"launch_site\": \"SHAR, Sriharikota, India\",\n", + " \"launch_vehicle\": \"GSLV-F04\",\n", + " \"orbit\": \"Geosynchronous (74\\u00b0 E)\",\n", + " \"mission_life\": \"12 Years\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-4B\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"3025 kg (at Lift \\u2013 off)\",\n", + " \"onboard_power\": \"5859 W\",\n", + " \"stabilization\": \"It uses 3 earth sensors, 2 digital sun sensors, 8 coarse analog sun sensors, 3 solar panel sun sensors and one sensor processing electronics. The wheels and wheel drive electronics were imported with indigenous wheel interface module to interface the wheel drive electronics and AOCE.\",\n", + " \"propulsion\": \"The propulsion system is employing 16 thrusters, 4 each located on east, west and AY sides and 2 each on north and south sides. There is one 440 N liquid apogee motor (using Mono Methyl Hydrazine (MMH) as fuel and oxides of Nitrogen (MON3 as oxidizer) and three pressurant tanks mounted on the LAM deck.\",\n", + " \"payload\": \"12 Ku band high power transponders covering Indian main land using 140W radiatively cooled TWTAs.\",\n", + " \"launch_date\": \"March 12, 2007\",\n", + " \"launch_site\": \"French Guiana\",\n", + " \"launch_vehicle\": \"Ariane5\",\n", + " \"orbit\": \"Geostationary (93.5o E Longitude)\",\n", + " \"mission_life\": \"12 Years\"\n", + " },\n", + " {\n", + " \"name\": \"CARTOSAT-2\",\n", + " \"id\": 1,\n", + " \"mission\": \"Remote Sensing\",\n", + " \"weight\": \"650 Kg\",\n", + " \"onboard_orbit\": \"900 Watts\",\n", + " \"stabilization\": \"3 - axis body stabilised using high torque reaction wheels, magnetic torquers and thrusters\",\n", + " \"payloads\": \"Panchromatic Camera\",\n", + " \"launch_date\": \"10 January 2007\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C7\",\n", + " \"orbit\": \"Polar Sun Synchronous\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-4A\",\n", + " \"id\": 1,\n", + " \"spacecraft_mass\": \"Lift off 3081 Kg Dry Mass 1386.55 Kg\",\n", + " \"orbit\": \"Geostationary ( 83o E)\",\n", + " \"power\": \"Solar Array to provide a power of 5922 W\",\n", + " \"battery\": \"Three 70 Ah Ni H2 Batteries for eclipse support of 4264 W\",\n", + " \"life\": \"12 Years\",\n", + " \"launch_date\": \"December 22, 2005\",\n", + " \"launch_vehicle\": \"ARIANE5-V169\"\n", + " },\n", + " {\n", + " \"name\": \"CARTOSAT-1\",\n", + " \"id\": 1,\n", + " \"launch_date\": \"5 May 2005\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C6\",\n", + " \"orbit\": \"618 km Polar Sun Synchronous\",\n", + " \"payloads\": \"PAN FORE, PAN - AFT\",\n", + " \"orbit_period\": \"97 min\",\n", + " \"number_of_orbits_per_day\": \"14\",\n", + " \"local_time_of_equator_crossing\": \"10:30 am\",\n", + " \"repetivity\": \"126 days\",\n", + " \"revisit\": \"5 days\",\n", + " \"lift-off_mass\": \"1560 kg\",\n", + " \"attitude_and_orbit_control\": \"3-axis body stabillised using reaction wheels, Magnetic Torquers and Hydrazine Thrusters\",\n", + " \"electrical_power\": \"15 sqm Solar Array generating 1100w, Two 24 Ah Ni-Cd batteries\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"HAMSAT\",\n", + " \"id\": 1,\n", + " \"launch_date\": \"May 5, 2005\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV-C6\",\n", + " \"orbit\": \"Geo-synchronous, 633.355 km (average)\",\n", + " \"payloads\": \"2 Transponders\"\n", + " },\n", + " {\n", + " \"name\": \"EDUSAT\",\n", + " \"id\": 1,\n", + " \"mission\": \"Education\",\n", + " \"spacecraft_mass\": \"1950.5 kg mass (at Lift - off) 819.4 kg (Dry mass)\",\n", + " \"onboard_power\": \"Total four solar panel of size 2.54 M x 1.525 M generating 2040 W (EOL), two 24 AH NiCd batteries for eclipse support\",\n", + " \"stabilization\": \"3 axis body stabilised in orbit using sensors, momentum and reaction wheels, magnetic torquers and eight 10 N & 22N reaction control thrusters.\",\n", + " \"propulsion\": \"440 N Liquid Apogee Motor with MON - 3 and MMH for orbit raising\",\n", + " \"payload\": \"Six upper extended C - band transponders Five lower Ku band transponders with regional beam coverage One lower Ku band National beam transponder with Indian main land coverage Ku beacon 12 C band high power transponders with extended coverage, covering southeast and northwest region apart from Indian main land using 63 W LTWTAs\",\n", + " \"launch_date\": \"September 20, 2004\",\n", + " \"launch_site\": \"SHAR, Sriharikota, India\",\n", + " \"launch_vehicle\": \"GSLV-F01\",\n", + " \"orbit\": \"Geostationary (74oE longitude)\",\n", + " \"mission_life\": \"7 Years (minimum)\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-P6 / RESOURCESAT-1\",\n", + " \"id\": 1,\n", + " \"launch_date\": \"October 17, 2003\",\n", + " \"launch_site\": \"SHAR, Sriharikota\",\n", + " \"launch_vehicle\": \"PSLV-C5\",\n", + " \"payloads\": \"LISS-4, LISS-3, AWiFS-A, AWiFS-B\",\n", + " \"orbit\": \"Polar Sun Synchronous\",\n", + " \"orbit_height\": \"817 km\",\n", + " \"orbit_inclination\": \"98.7o\",\n", + " \"orbit_period\": \"101.35 min\",\n", + " \"number_of_orbits_per_day\": \"14\",\n", + " \"local_time_of_equator_crossing\": \"10:30 am\",\n", + " \"repetivity_(liss-3)\": \"24 days\",\n", + " \"revisit\": \"5 days\",\n", + " \"lift-off_mass\": \"1360 kg\",\n", + " \"attitude_and_orbit_control\": \"3-axis body stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters\",\n", + " \"power\": \"Solar Array generating 1250 W, Two 24 Ah Ni-Cd batteries\",\n", + " \"mission_life\": \"5 years\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-3E\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"spacecraft_mass\": \"2,775 kg (Mass at Lift-off) 1218 kg (Dry mass)\",\n", + " \"launch_date\": \"September 28, 2003\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane5-V162\",\n", + " \"orbit\": \"Geostationary Orbit\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-2\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"1800 kg\",\n", + " \"launch_date\": \"May 8, 2003\",\n", + " \"launch_site\": \"SHAR, Sriharikota, India\",\n", + " \"launch_vehicle\": \"GSLV\\u2013D2\",\n", + " \"orbit\": \"Geostationary orbit (48oE longitude)\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-3A\",\n", + " \"id\": 1,\n", + " \"mission\": \"Telecommunication, broadcasting and Meteorology\",\n", + " \"spacecraft_mass\": \"2,950 kg (Mass at Lift\\u2013off) 1,348 kg (Dry mass)\",\n", + " \"onboard_power\": \"3,100 W\",\n", + " \"stabilization\": \"3 \\u2013 axis body stabilised in orbit using momentum and reaction wheels, solar flaps, magnetic torquers and eight 10 N and eight 22 N reaction control thrusters\",\n", + " \"propulsion\": \"440 N Liquid Apogee Motor with MON-3 (Mixed Oxides of Nitrogen) and MMH (Mono Methyl Hydrazine) for orbit raising\",\n", + " \"payload\": \"Communication payload - 12 C \\u2013 band transponders, - 6 upper extended C band transponders - 6 Ku band transponders - 1 Satellite Aided Search & Rescue transponders Meteorological payload - Very High Resolution Radiometer (VHRR) with 2 km resolution in visible band and 8 km resolution in infrared and water vapour band - Charged Coupled Device (CCD) camera operating in visible, near infrared and shortwave infrared band with 1 km resolution. - Data Relay Transponders (DRT)\",\n", + " \"launch_date\": \"April 10, 2003\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane5-V160\",\n", + " \"orbit\": \"Geostationary (93.5o E longitude)\",\n", + " \"mission_life\": \"12 Years\"\n", + " },\n", + " {\n", + " \"name\": \"KALPANA-1\",\n", + " \"id\": 1,\n", + " \"mission\": \"7 Years\",\n", + " \"spacecraft_mass\": \"1060 kg mass (at Lift \\u2013 off) 498 kg (Dry mass)\",\n", + " \"onboard_power\": \"550 W\",\n", + " \"payload\": \"Very High Resolution Radiometer (VHRR) Data Relay Transponder (DRT)\",\n", + " \"launch_date\": \"12 September 2002\",\n", + " \"launch_site\": \"SHAR, Sriharikota\",\n", + " \"launch_vehicle\": \"PSLV \\u2013 C4\",\n", + " \"orbit\": \"Geostationary (74 deg East longitude)\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-3C\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication, broadcasting and Meteorology\",\n", + " \"spacecraft_mass\": \"2,650 kg (Mass at Lift - off) 1218 kg (Dry mass)\",\n", + " \"onboard_power\": \"2765 W\",\n", + " \"propulsion\": \"Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.\",\n", + " \"payload\": \"24 C band transponders 6 Extended C - band Transponders 2 S - band Transponders\",\n", + " \"launch_date\": \"January 24, 2002\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane5-V147\",\n", + " \"orbit\": \"Geostationary (74o longitude)\",\n", + " \"mission_life\": \"Very long\"\n", + " },\n", + " {\n", + " \"name\": \"The Technology Experiment Satellite\\n (TES)\",\n", + " \"id\": 1,\n", + " \"launch_date\": \"22 October 2001\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C3\",\n", + " \"orbit\": \"572 km Sun Synchronous\",\n", + " \"payloads\": \"PAN\"\n", + " },\n", + " {\n", + " \"name\": \"PSLV-C3 / TES\",\n", + " \"id\": 1,\n", + " \"launch_date\": \"22 October 2001\",\n", + " \"launch_site\": \"SHAR Centre Sriharikota India\",\n", + " \"launch_vehicle\": \"PSLV- C3\",\n", + " \"orbit\": \"572 km Sun Synchronous\",\n", + " \"payloads\": \"PAN\"\n", + " },\n", + " {\n", + " \"name\": \"GSAT-1\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"1530 kg\",\n", + " \"launch_date\": \"18 April 2001\",\n", + " \"launch_site\": \"SHAR, Sriharikota\",\n", + " \"launch_vehicle\": \"GSLV \\u2013 D1\",\n", + " \"orbit\": \"Sun Synchronous Geo stationary orbit\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-3B\",\n", + " \"id\": 1,\n", + " \"mission\": \"Very long\",\n", + " \"spacecraft_mass\": \"2,070 (Mass at Lift \\u2013 off) 970 kg (Dry mass)\",\n", + " \"onboard_power\": \"1,712 W\",\n", + " \"stabilization\": \"3 \\u2013 axis body stabilised biased momentum control system using earth sensors, sun sensors, inertial reference unit, momentum / reaction wheels, magnetic torquers and unified bi-propellant thrusters.\",\n", + " \"propulsion\": \"Liquid Apogee Motor with fuel and oxidizer stored in separate titanium tanks and pressurant in Kevlar wound titanium tank.\",\n", + " \"payload\": \"12 extended C \\u2013 band Transponders Five Ku band Transponders Mobile Satellite Services (MSS)\",\n", + " \"launch_date\": \"22nd March 2000\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane -5\",\n", + " \"orbit\": \"Geostationary (83 deg East longitude)\",\n", + " \"inclination\": \"7 deg\"\n", + " },\n", + " {\n", + " \"name\": \"Oceansat(IRS-P4)\",\n", + " \"id\": 1,\n", + " \"launch_date\": \"May 26, 1999\",\n", + " \"launch_site\": \"SHAR, Sriharikota\",\n", + " \"launch_vehicle\": \"PSLV - C2\",\n", + " \"orbit\": \"Polar Sun Synchronous\",\n", + " \"altitude\": \"720 km\",\n", + " \"inclination\": \"98.28 deg\",\n", + " \"period\": \"99.31 min\",\n", + " \"local_time_of_eq._crossing\": \"12 noon\",\n", + " \"repetitivity_cycle\": \"2 days\",\n", + " \"size\": \"2.8m x 1.98m x 2.57m\",\n", + " \"mass_at_lift_off\": \"1050 kg\",\n", + " \"length_when_fully_deployed\": \"11.67 m\",\n", + " \"attitude_and_orbit_control\": \"3-axis body-stabilised using Reaction Wheels, Magnetic Torquers and Hydrazine Thrusters\",\n", + " \"power\": \"9.6 Sq.m Solar Array generating 750w Two 21 Ah Ni-Cd Batteries\",\n", + " \"mission_completed_on\": \"August 8, 2010\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-2E\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication and Meteorology\",\n", + " \"spacecraft_mass\": \"2,550 kg (Mass at Lift-off) 1150 kg (Dry mass)\",\n", + " \"launch_date\": \"03 April 1999\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane \\u2013 42P\",\n", + " \"orbit\": \"Geosynchronous (83 deg east longitude)\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-1D\",\n", + " \"id\": 1,\n", + " \"mission\": \"Operational Remote Sensing\",\n", + " \"weight\": \"1250 kg\",\n", + " \"onboard_power\": \"809 Watts (generated by 9.6 sq.metres Solar Panels)\",\n", + " \"communication\": \"S-band, X-band\",\n", + " \"stabilization\": \"Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer\",\n", + " \"rcs\": \"Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters\",\n", + " \"payload\": \"Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)\",\n", + " \"onboard_tape_recorder\": \"Storage Capacity : 62 G bits\",\n", + " \"launch_date\": \"December 28, 1995\",\n", + " \"launch_site\": \"Baikanur Cosmodrome Kazakhstan\",\n", + " \"launch_vehicle\": \"Molniya\",\n", + " \"orbit\": \"817 km Polar Sun-synchronous\",\n", + " \"inclination\": \"98.69o\",\n", + " \"repetivity\": \"24 days\",\n", + " \"local_time\": \"10.30 a.m\",\n", + " \"mission_completed_on\": \"September 21, 2007\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-2D\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"2079 kg with propellants, 995 kg dry weight\",\n", + " \"onboard_power\": \"1650 Watts\",\n", + " \"communication\": \"C, extended C, S and Ku bands\",\n", + " \"stabilization\": \"Three axis stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers\",\n", + " \"propulsion\": \"Integrated bipropellan stystem ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.\",\n", + " \"payload\": \"Transponders: 16C-band / extended C-band transponders (forFSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders\",\n", + " \"launch_date\": \"June 4, 1997\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Arianev 4\",\n", + " \"orbit\": \"Geostationary 93,.5deg.E\",\n", + " \"inclination\": \"0 deg.\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-P3\",\n", + " \"id\": 1,\n", + " \"mission\": \"Remote sensing of earth's natural resources. Study of X-ray Astronomy. Periodic calibration of PSLV tracking radar located at tracking stations.\",\n", + " \"weight\": \"920 kg\",\n", + " \"onboard_power\": \"817 Watts\",\n", + " \"communication\": \"S-band\",\n", + " \"stabilization\": \"Three axis body stabilized\",\n", + " \"rcs\": \"Combinations of bladder type and surface tension type mass expulsion monopropellant hydrazine system\",\n", + " \"payload\": \"WideField Sensor (WiFS), Modular Opto - electronic Scanner (MOS), Indian X-ray Astronomy Experiment (IXAE), C-band transponder(CBT)\",\n", + " \"launch_date\": \"March 21, 1996\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV-D3\",\n", + " \"orbit\": \"817 km. Circular polar sun-synchronous with equatorial crossing at 10.30 am (descending node)\",\n", + " \"inclination\": \"98.68o\",\n", + " \"repetivity\": \"WiFS : 5 days\",\n", + " \"mission_completed_during\": \"January 2006\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-1C\",\n", + " \"id\": 1,\n", + " \"mission\": \"Operational Remote Sensing\",\n", + " \"weight\": \"1250 kg\",\n", + " \"onboard_power\": \"809 Watts (generated by 9.6 sq.metres Solar Panels)\",\n", + " \"communication\": \"S-band, X-band\",\n", + " \"stabilization\": \"Three axis body stabilized (zero momentum) with 4 Reaction Wheels, Magnetic torquer\",\n", + " \"rcs\": \"Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters\",\n", + " \"payload\": \"Three solid state Push Broom Cameras: PAN (<6 metre solution )LlSS-3(23.6 metre resolution) and WiFS (189 metre resolution)\",\n", + " \"onboard_tape_recorder\": \"Storage Capacity : 62 G bits\",\n", + " \"launch_date\": \"December 28, 1995\",\n", + " \"launch_site\": \"Baikanur Cosmodrome Kazakhstan\",\n", + " \"launch_vehicle\": \"Molniya\",\n", + " \"orbit\": \"817 km Polar Sun-synchronous\",\n", + " \"inclination\": \"98.69o\",\n", + " \"repetivity\": \"24 days\",\n", + " \"local_time\": \"10.30 a.m\",\n", + " \"mission_completed_on\": \"September 21, 2007\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-2C\",\n", + " \"id\": 1,\n", + " \"mission\": \"Communication\",\n", + " \"weight\": \"2106 kg with propellants 946 kg dry weight\",\n", + " \"onboard_power\": \"1320 Watts\",\n", + " \"communication\": \"C extended C, S and Ku bands\",\n", + " \"stabilization\": \"Three axis stabilized with two Momen'tum Wheels & one Reaction Wheel, Magnetic torquers\",\n", + " \"propulsion\": \"Integrated bipropellant system ( MMH and N2 04) With sixteen 22N thrusters and 440N LAM.\",\n", + " \"payload\": \"Transponders: 16C-band / extended C-band transponders (for FSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders\",\n", + " \"launch_date\": \"December 7, 1995\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane4\",\n", + " \"orbit\": \"Geostationary 93.5 deg E\",\n", + " \"inclination\": \"0 deg.\",\n", + " \"mission_life\": \"Seven years(nominal)\",\n", + " \"orbit_life\": \"Very Long\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-P2\",\n", + " \"id\": 1,\n", + " \"mission\": \"Operational Remote Sensing\",\n", + " \"weight\": \"804 kg\",\n", + " \"onboard_power\": \"510 Watts\",\n", + " \"communication\": \"S-band, X-band\",\n", + " \"stabilization\": \"Three axis body stabilized with 4 Reaction Wheels, Magnetic torquers\",\n", + " \"rcs\": \"4 tanks containing Monopropellant Hydrazine based with sixteen 1 N thrusters and one 11 N thruster\",\n", + " \"payload\": \"Two solid state Push Broom Cameras operating in four spectral bands in the visible and near-IR range using CCD arrays: LlSS-2A & LlSS-2B (Resolution: 32.74 metre)\",\n", + " \"launch_date\": \"October 15, 1994\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV-D2\",\n", + " \"inclination\": \"98.68o\",\n", + " \"repetivity\": \"24 days\",\n", + " \"mission_completed_on\": \"1997\"\n", + " },\n", + " {\n", + " \"name\": \"SROSS-C2\\n \",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"115 kg\",\n", + " \"onboard_power\": \"45 Watts\",\n", + " \"communication\": \"S-band and VHF\",\n", + " \"rcs\": \"Monopropellant Hydrazine based with six 1 Newton thrusters\",\n", + " \"payload\": \"Gamma Ray Burst (GRB) & Retarding Potential Analyser (RPA)\",\n", + " \"launch_date\": \"May 04,1994\",\n", + " \"launch_site\": \"SHAR Centre,Sriharikota,India\",\n", + " \"launch_vehicle\": \"Augmented Satellite Launch Vehicle (ASLV)\",\n", + " \"orbit\": \"430 x 600 km.\",\n", + " \"inclination\": \"45 deg.\",\n", + " \"mission_life\": \"Six months (nominal)\",\n", + " \"orbital_life\": \"Two years (nominal)\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-1E\",\n", + " \"id\": 1,\n", + " \"mission\": \"Operational Remote Sensing\",\n", + " \"weight\": \"846 kg\",\n", + " \"onboard_power\": \"415 Watts\",\n", + " \"communication\": \"S-band (TIC) & VHF\",\n", + " \"stabilization\": \"Three axis body stabilized ( zero momentum) with 4 Reaction Wheels, Magnetic torquers\",\n", + " \"rcs\": \"Monopropellant Hydrazine based RCS with 1 Newton thrusters ( 16 Nos.)\",\n", + " \"payload\": \"LlSS-1 MEOSS (Mono-ocula Erlectro Optic Stereo Scanner)\",\n", + " \"launch_date\": \"September 20, 1993\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"PSLV-D1\",\n", + " \"orbit\": \"Not realised\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-2B\",\n", + " \"id\": 1,\n", + " \"mission\": \"Multipurpose Communication, meteorology and Satellite based search and rescue\",\n", + " \"weight\": \"1906 kg with propellant 916 kg dry weight\",\n", + " \"onboard_power\": \"One KW approx.\",\n", + " \"communication\": \"C, extended C and S band\",\n", + " \"stabilization\": \"Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers\",\n", + " \"propulsion\": \"Integrated bipropellant system ( MMH and N2 04) With sixteen 22 N thrusters and 440 N LAM.\",\n", + " \"payload\": \"Transponders: 12C-band (for FSS),6 ext. C-band (for FSS) 2S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band\",\n", + " \"launch_date\": \"July 23, 1993\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane 4\",\n", + " \"orbit\": \"Geostationary 93.5o E\",\n", + " \"inclination\": \"0o\",\n", + " \"mission_life\": \"Seven years(nominal)\",\n", + " \"orbit_life\": \"Very Long\"\n", + " },\n", + " {\n", + " \"name\": \"INSAT-2A\",\n", + " \"id\": 1,\n", + " \"mission\": \"Multipurpose Communication, meteorology and Satellite based search and rescue\",\n", + " \"weight\": \"1906 kg with propellant 916 kg dry weight\",\n", + " \"onboard_power\": \"One KW approx\",\n", + " \"communication\": \"C, extended C and S band\",\n", + " \"stabilization\": \"Three axis body stabilized with two Momentum Wheels & one Reaction Wheel, Magnetic torquers\",\n", + " \"propulsion\": \"Integrated bipropellant system (MMH and N2 04) With sixteen 22 N thrusters and 440 LAM.\",\n", + " \"payload\": \"Transponders: 12 C-band (for FSS),6 ext. C-band (for FSS) 2 S-band (for BSS),1Data relay transponder (for met.data), 1 transponder for research and rescue, Very High Resolution radiometer (VHRR) for\\u00a0meteorological observation with 2 km resolution in the visible and 8 km resolution in the IR band\",\n", + " \"launch_date\": \"July 10,1992\",\n", + " \"launch_site\": \"French Guyana\",\n", + " \"launch_vehicle\": \"Ariane 4\",\n", + " \"orbit\": \"Geostationary 74oE longitude\",\n", + " \"inclination\": \"0o\",\n", + " \"mission_life\": \"Seven years(nominal)\",\n", + " \"orbit_life\": \"Very Long\"\n", + " },\n", + " {\n", + " \"name\": \"SROSS-C\\n\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"106.1 kg\",\n", + " \"onboard_power\": \"45 Watts\",\n", + " \"communication\": \"S-band and VHF\",\n", + " \"stabilization\": \"Spin stabilized with a Magnetic Torquer and Magnetic Bias Control\",\n", + " \"payload\": \"Gamma Ray Burst (GRB) experiment & Retarding Potential Analyser (RPA) experiment\",\n", + " \"launch_date\": \"May 20,1992\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"Augmented Satellite Launch Vehicle (ASLV)\",\n", + " \"orbit\": \"267 x 391 km\",\n", + " \"mission_life\": \"Two months (Re-entered on July15,1992)\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-1B\",\n", + " \"id\": 1,\n", + " \"mission\": \"Operational Remote Sensing\",\n", + " \"weight\": \"975 kg\",\n", + " \"onboard_power\": \"600 Watts\",\n", + " \"communication\": \"S-band, X-band and VHF (commanding only)\",\n", + " \"stabilization\": \"Three axis body stabilized (zero momentum) with 4 Reactions Wheels, Magnetic torquers\",\n", + " \"rcs\": \"Monopropellant Hydrazine based with sixteen 1 Newton thrusters\",\n", + " \"payload\": \"Three solid state Push Broom Cameras LlSS-1 (72.5 metre resolution), LlSS-2A and LlSS-2B (36.25 metre resolution)\",\n", + " \"launch_date\": \"August 29, 1991\",\n", + " \"launch_site\": \"Baikanur Cosmodrome Kazakhstan\",\n", + " \"launch_vehicle\": \"Vostok\",\n", + " \"orbit\": \"904 km Polar Sun Synchronous\",\n", + " \"inclination\": \"99.08o\",\n", + " \"repetivity\": \"22 days\",\n", + " \"local_time\": \"10.30 a.m. (descending node)\",\n", + " \"mission_completed_on\": \"December 20, 2003\"\n", + " },\n", + " {\n", + " \"name\": \"SROSS-2\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"150 kg\",\n", + " \"onboard_power\": \"90 Watts\",\n", + " \"communication\": \"S-band and VHF\",\n", + " \"stabilization\": \"Three axis body stabilized (biased momentum) with a Momentum Wheel and Magnetic Torquer\",\n", + " \"propulsion_system\": \"Monopropellant (Hydrazine based) Reaction Control System\",\n", + " \"payload\": \"Gamma Ray Burst (GRB) payload and Mono Payload Ocular Electro-Optic Stereo Scanner (MEOSS) built by DLR, Germany\",\n", + " \"launch_date\": \"July 13, 1988\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"Augmented Satellite Launch Vehicle (ASLV)\",\n", + " \"orbit\": \"Not realised\"\n", + " },\n", + " {\n", + " \"name\": \"IRS-1A\",\n", + " \"id\": 1,\n", + " \"mission\": \"Operational Remote Sensing\",\n", + " \"weight\": \"975 kg\",\n", + " \"onboard_power\": \"600 Watts\",\n", + " \"communication\": \"S-band, X-band and VHF(commanding only)\",\n", + " \"stabilization\": \"Three axis body stabilized (zero momentum) with 4 Reactions Wheels, Magnetic torquers\",\n", + " \"rcs\": \"Monopropellant Hydrazine based with sixteen 1 Newton thrusters\",\n", + " \"payload\": \"Three solid state Push Broom Cameras: LISS-1(72.5 metre resolution), LISS-2A and LISS-2B (36.25 metre resolution)\",\n", + " \"launch_date\": \"March 17, 1988\",\n", + " \"launch_site\": \"Baikanur Cosmodrome Kazakhstan\",\n", + " \"launch_vehicle\": \"Vostok\",\n", + " \"orbit\": \"904 km Polar Sun-synchronous\",\n", + " \"inclination\": \"99.08o\",\n", + " \"repetivity\": \"22 days (307 orbits)\",\n", + " \"local_time\": \"10.30 a.m. (descending node)\",\n", + " \"mission_completed_during\": \"July 1996\"\n", + " },\n", + " {\n", + " \"name\": \"SROSS-1\\n\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"150 kg\",\n", + " \"onboard_power\": \"90 Watts\",\n", + " \"communication\": \"S-band and VHF\",\n", + " \"stabilization\": \"Three axis body stabilized (biased momentum) with a Momentum Wheel and Magnetic Torquer\",\n", + " \"propulsion_system\": \"Monopropellant (Hydrazine based) Reaction control system\",\n", + " \"payload\": \"Launch Vehicle Monitoring Platform(LVMP), Gamma Ray Burst (GRB) payload and Corner Cube Retro Reflector (CCRR) for laser tracking\",\n", + " \"launch_date\": \"March 24, 1987\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"Augmented Satellite Launch Vehicle (ASLV)\",\n", + " \"orbital_life\": \"Not realised\"\n", + " },\n", + " {\n", + " \"name\": \"Rohini Satellite RS-D2\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"41.5 kg\",\n", + " \"onboard_power\": \"16 Watts\",\n", + " \"communication\": \"VHF band\",\n", + " \"stabilization\": \"Spin stabilized\",\n", + " \"payload\": \"Smart sensor (remote sensing payload), L-band beacon\",\n", + " \"launch_date\": \"April 17, 1983\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"SLV-3\",\n", + " \"orbit\": \"371 x 861 km\",\n", + " \"inclination\": \"46o\",\n", + " \"mission_life\": \"17 months\",\n", + " \"orbital_life\": \"Seven years (Re-entered on April 19, 1990)\"\n", + " },\n", + " {\n", + " \"name\": \"Bhaskara-II\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental Remote Sensing\",\n", + " \"weight\": \"444 kg\",\n", + " \"onboard_power\": \"47 Watts\",\n", + " \"communication\": \"VHF band\",\n", + " \"stabilization\": \"Spin stabilized (spin axis controlled)\",\n", + " \"payload\": \"TV cameras, three band Microwave Radiometer (SAMIR)\",\n", + " \"launch_date\": \"Nov 20, 1981\",\n", + " \"launch_site\": \"Volgograd Launch Station (presently in Russia)\",\n", + " \"launch_vehicle\": \"C-1 Intercosmos\",\n", + " \"orbit\": \"541 x 557 km\",\n", + " \"inclination\": \"50.7o\",\n", + " \"mission_life\": \"One year (nominal)\",\n", + " \"orbital_life\": \"About 10 years ( Re-entered in 1991 )\"\n", + " },\n", + " {\n", + " \"name\": \"APPLE\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental geostationary communication\",\n", + " \"weight\": \"670 kg\",\n", + " \"onboard_power\": \"210 Watts\",\n", + " \"communication\": \"VHF and C-band\",\n", + " \"stabilization\": \"Three axis stabilized (biased momentum) with Momentum Wheels, Torquers & \\u00a0Hydrazine based Reaction control system\",\n", + " \"payload\": \"C - band transponders (Two)\",\n", + " \"launch_date\": \"June19,1981\",\n", + " \"launch_site\": \"Kourou (CSG), French Guyana\",\n", + " \"launch_vehicle\": \"Ariane -1(V-3)\",\n", + " \"orbit\": \"Geosynchronous (102 deg. E\\u00a0 longitude, over Indonesia)\",\n", + " \"inclination\": \"Near zero\",\n", + " \"mission_life\": \"Two years\"\n", + " },\n", + " {\n", + " \"name\": \"Rohini Satellite RS-D1\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"38 kg\",\n", + " \"onboard_power\": \"16 Watts\",\n", + " \"communication\": \"VHF band\",\n", + " \"stabilization\": \"Spin stabilized\",\n", + " \"payload\": \"Landmark Tracker ( remote sensing payload)\",\n", + " \"launch_date\": \"May 31,1981\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"SLV-3\",\n", + " \"orbit\": \"186 x 418 km (achieved)\",\n", + " \"inclination\": \"46 deg\",\n", + " \"orbital_life\": \"Nine days\"\n", + " },\n", + " {\n", + " \"name\": \"Rohini Satellite RS-1\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"35 kg\",\n", + " \"onboard_power\": \"16 Watts\",\n", + " \"communication\": \"VHF band\",\n", + " \"stabilization\": \"Spin stabilized\",\n", + " \"payload\": \"Launch vehicle monitoring instruments\",\n", + " \"launch_date\": \"July 18,1980\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"SLV-3\",\n", + " \"orbit\": \"305 x 919 km\",\n", + " \"inclination\": \"44.7 deg.\",\n", + " \"mission_life\": \"1.2 years\",\n", + " \"orbital_life\": \"20 months\"\n", + " },\n", + " {\n", + " \"name\": \"Rohini Technology Payload\\n (RTP)\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental\",\n", + " \"weight\": \"35 kg\",\n", + " \"onboard_power\": \"3 Watts\",\n", + " \"communication\": \"VHF band\",\n", + " \"stabilization\": \"Spin stabilized (spin axis controlled)\",\n", + " \"payload\": \"Launch vehicle monitoring instruments\",\n", + " \"launch_date\": \"August 10,1979\",\n", + " \"launch_site\": \"SHAR Centre, Sriharikota, India\",\n", + " \"launch_vehicle\": \"SLV-3\",\n", + " \"orbit\": \"Not achieved\"\n", + " },\n", + " {\n", + " \"name\": \"Bhaskara-I\",\n", + " \"id\": 1,\n", + " \"mission\": \"Experimental Remote Sensing\",\n", + " \"weight\": \"442 kg\",\n", + " \"onboard_power\": \"47 Watts\",\n", + " \"communication\": \"VHF band\",\n", + " \"stabilization\": \"Spin stabilized (spin axis controlled)\",\n", + " \"payload\": \"TVcameras, three band Microwave Radiometer (SAMIR)\",\n", + " \"launch_date\": \"Jun 07,1979\",\n", + " \"launch_site\": \"Volgograd Launch Station (presently in Russia)\",\n", + " \"launch_vehicle\": \"C-1Intercosmos\",\n", + " \"orbit\": \"519 x 541 km\",\n", + " \"inclination\": \"50.6 deg\",\n", + " \"mission_life\": \"One year (nominal)\",\n", + " \"orbital_life\": \"About 10 years ( Re-entered in 1989 )\"\n", + " },\n", + " {\n", + " \"name\": \"Aryabhata \",\n", + " \"id\": 1,\n", + " \"mission\": \"Scientific/ Experimental\",\n", + " \"weight\": \"360 kg\",\n", + " \"on_board_power\": \"46 Watts\",\n", + " \"communication\": \"VHF band\",\n", + " \"stabilization\": \"Spinstabilize\",\n", + " \"payload\": \"X-ray Astronomy Aeronomy & Solar Physics\",\n", + " \"launch_date\": \"April 19, 1975\",\n", + " \"launch_site\": \"Volgograd Launch Station (presently in Russia)\",\n", + " \"launch_vehicle\": \"C-1 Intercosmos\",\n", + " \"orbit\": \"563 x 619 km\",\n", + " \"inclination\": \"50.7 deg\",\n", + " \"mission_life\": \"6 months(nominal), Spacecraft mainframe active till March,1981\",\n", + " \"orbital_life\": \"Nearly seventeen years (Re-entered on February 10,1992)\"\n", + " }\n", + "]\n" + ] + } + ], + "source": [ + "\n", + "data = []\n", + "for spacecraft in spacecrafts:\n", + " title = spacecraft.text\n", + " link = spacecraft[\"href\"]\n", + " url = \"https://www.isro.gov.in/{craft}\".format(craft=link)\n", + " response = requests.get(url)\n", + " soup = BeautifulSoup(response.text,'lxml')\n", + " tables = soup.find_all(\"table\", {\"class\":\"pContent table table-striped table-bordered\"})\n", + " count = 0\n", + " for table in tables:\n", + " rows = table.find_all('tr')\n", + " dt = {\"name\":title,\"id\":1}\n", + " for row in rows:\n", + " cols = row.find_all('td')\n", + " cols = [ele.text.strip() for ele in cols]\n", + " if(len(cols)== 2):\n", + " dt[\"\".join(\"_\".join(cols[0].lower().split(\" \")).split(\"\\n\"))] = (\" \".join((cols[1]).split(\"\\n\"))).strip()\n", + "\n", + " data.append(dt)\n", + "\n", + "\n", + "data = data.reverse\n", + "for i in range(len(data)):\n", + " data[i][\"id\"] = i+1\n", + "\n", + "json_data = json.dumps(data,indent=2)\n", + "print(json_data)\n", + "\n", + "\n", + "\n", + "\n" + ] + }, + { + "cell_type": "code", + "execution_count": null, + "metadata": {}, + "outputs": [], + "source": [ + "\n" + ] + } + ], + "metadata": { + "kernelspec": { + "display_name": "Python 3", + "language": "python", + "name": "python3" + }, + "language_info": { + "codemirror_mode": { + "name": "ipython", + "version": 3 + }, + "file_extension": ".py", + "mimetype": "text/x-python", + "name": "python", + "nbconvert_exporter": "python", + "pygments_lexer": "ipython3", + "version": "3.11.2" + }, + "orig_nbformat": 4 + }, + "nbformat": 4, + "nbformat_minor": 2 +}