Mission type | Communications, Cloud Observation |
---|---|
Operator | INSAT |
COSPAR ID | 1990-051A |
SATCAT no. | 20643 |
Mission duration | 7 years |
Spacecraft properties | |
Spacecraft type | INSAT-1 |
Manufacturer | Ford Aerospace |
Launch mass | 1,190 kilograms (2,620 lb) (Lift - off Mass)[1] |
Dry mass | 550 kilograms (1,210 lb)[1] |
Power | 1000 W (Solar array);[1] Nominal Power: 1200.0 W [2] |
Start of mission | |
Launch date | June 12, 1990, 05:52:00 UTC [3][4] |
Rocket | Delta 4925[5] |
Launch site | Cape Canaveral LC-17B |
Contractor | NASA |
Deployment date | UTC |
End of mission | |
Disposal | Decommissioned (mission life over)[1] |
Deactivated | 14 May 2002 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geostationary |
Longitude | 83° east [1] |
Semi-major axis | 42,164.88 kilometres (26,200.04 mi) |
Eccentricity | 0.0012393 |
Perigee altitude | 35,741 kilometres (22,208 mi) |
Apogee altitude | 35,846 kilometres (22,274 mi) |
Inclination | 14.30 degrees[6] |
Period | 23.93 hours |
Epoch | 14 November 2013, 15:52:38 UTC[6] |
INSAT-1D was 4th and the concluding multipurpose geostationary satellite of the INSAT-1 (first-generation seven-year responsibility for the operation of the INSAT space segment.[7]
But the success of this launch meant a lot to India - a country that was setting up its national computer networks. Relying on a lot of communication circuits, microwave, coaxial, and fibre-optic telecommunication links throughout the country causes a huge problem; and thus the Indian Space Research Organisation (ISRO) planned at the start of the INSAT-1 series to always have at least two satellites in space to meet the increasing demand of telecommunication links for India's civilian community. INSAT-1A and INSAT-1C had already faced immature death and their plans had suffered a serious setback. Another satellite INSAT-1B, launched in 1983, exceeded its planned seven-year working life.[8]
COSPAR ID: 1990-051A
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