Mission type | Communications Weather |
---|---|
Operator | INSAT |
COSPAR ID | 2003-013A |
SATCAT no. | 27714 |
Website | INSAT 3A |
Spacecraft properties | |
Manufacturer | ISRO |
Launch mass | 2,950 kilograms (6,500 lb) |
Dimensions | 2.8 x 1.7 x 2.0 metres |
Power | 3.1 kilowatts |
Start of mission | |
Launch date | 9 April 2003, 22:52 UTC |
Rocket | Ariane 5G V160 |
Launch site | Kourou ELA-3 |
Contractor | Arianespace |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 93.5° East ( 0°00′N93°30′E / 0°N +93.5°E ) |
Inclination | 74 degrees |
Period | 12 years |
INSAT-3A, a multipurpose satellite built by ISRO was launched by Ariane in April 2003. It is located at 93.5 degree East longitude. It is third satellite in INSAT-3 series after INSAT-3B & INSAT-3C. Built at a cost of $53 mn, it provides communication, weather, and search and rescue services.
INSAT 3A was launched by Ariane-5 launch vehicle of Arianespace on April 9, 2003, at 22.52 UTC from Kourou, French Guiana. [1] It was placed into a Geosynchronous Transfer Orbit (GTO), 30 minutes after the lift-off in 3-axis stabilized mode, with a perigee (nearest point to earth) of 859 km and an apogee (farthest point to earth) of 36,055 km and an inclination of 1.99 degrees with respect to the equator. [2] Its co-passenger on its launch was GALAXI-XII of PanAmSat. Its Master Control Facility (MCF) is located at Hassan, Karnataka (India). It is 3-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. Its propulsion system consists of 440 N Liquid Apogee Motor MON-3 (Mixed Oxides of Nitrogen) and MMH (MonoMethylHydrazine) for orbit raising.
The satellite raised its orbit to GEO and arrived in the 93.5 degree East longitude orbital location. [3] It joined INSAT-3B and INSAT-3C which were already in orbit operating from a similar orbital location. [4]
The INSAT-3A communications payload consists of: [5]
The INSAT-3A meteorological payload consists of [5]
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