INSAT-1B
INSAT | ||
COSPAR ID | 1983-089B | |
---|---|---|
SATCAT no. | 14318 | |
Mission duration | 7 years | |
Spacecraft properties | ||
Spacecraft type | INSAT-1 | |
Manufacturer | Ford Aerospace | |
Launch mass | 1,152 kilograms (2,540 lb) | |
Start of mission | ||
Launch date | 30 August 1983, 06:32:00 UTC[1] | |
Rocket | Space Shuttle Challenger STS-8 / PAM-D | |
Launch site | Kennedy LC-39A | |
Contractor | NASA | |
Deployment date | 31 August 1983, 07:48 | UTC|
End of mission | ||
Disposal | Decommissioned | |
Deactivated | August 1993 | |
Orbital parameters | ||
Reference system | 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 | 14.69 degrees | |
Period | 23.93 hours | |
Epoch | 14 November 2013, 15:52:38 UTC[2] | |
INSAT-1B was an Indian
Built by
INSAT-1B was deployed by
After some initial problems deploying its solar array,[6] INSAT-1B became operational in October 1983. It was located at 74° east for most of its operational life, before being moved to 93° east in 1992. In August 1993 it was decommissioned and raised to a graveyard orbit slightly above geosynchronous altitude.[3] As of 14 November 2013, it is in an orbit with a perigee of 35,741 kilometres (22,208 mi), an apogee of 35,846 kilometres (22,274 mi), inclination of 14.69 degrees and an orbital period of 23.93 hours.[2]
References
- ^ a b McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 16 November 2013.
- ^ a b "INSAT 1B Satellite details 1983-089B NORAD 14318". N2YO. 14 November 2013. Retrieved 16 November 2013.
- ^ a b c d e Krebs, Gunter. "Insat 1A, 1B, 1C, 1D". Gunter's Space Page. Retrieved 16 November 2013.
- ISBN 0-387-21519-0.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 16 November 2013.
- ISBN 0-387-21519-0.