SBS 2 (satellite)
| Mission type | Communications | 
|---|---|
| Operator | SBS | 
| COSPAR ID | 1981-096A | 
| SATCAT no. | 12855 | 
| Mission duration | 7 years design life | 
| Spacecraft properties | |
| Bus | HS-376 | 
| Manufacturer | Hughes Space and Communications | 
| Launch mass | 550 kilograms (1,210 lb) | 
| Start of mission | |
| Launch date | 24 September 1981, 23:09 UTC | 
| Rocket | Delta-3910 PAM-D | 
| Launch site | Cape Canaveral LC-17A | 
| Contractor | NASA | 
| End of mission | |
| Disposal | Decommissioned | 
| Deactivated | September 1996 | 
| Orbital parameters | |
| Reference system | Geocentric | 
| Regime | Geostationary | 
| Longitude | 117° W[1] | 
| Eccentricity | 0.73679 | 
| Perigee altitude | 166 kilometres (103 mi) | 
| Apogee altitude | 36,830 kilometres (22,890 mi) | 
| Inclination | 27.7° | 
| Period | 650.8 minutes | 
| Epoch | September 24, 1981 | 
| Transponders | |
| Band | 14 Ku band | 
SBS 2 was a geostationary communications satellite designed and manufactured by Hughes (now Boeing) on the HS-376 platform. It was ordered by Satellite Business Systems, which later sold it to Hughes Communications. It had a Ku band payload and operated on the 117°W longitude.[2]
Satellite description
The spacecraft was designed and manufactured by Hughes on the HS-376 satellite bus. It had a launch mass of 550 kg (1,210 lb), a geostationary orbit and a 7-year design life.[3]
History
On September 24, 1981, SDS 2 was finally launched by a Delta-3910 PAM-D from Cape Canaveral at 23:09 UTC.
In April 1996, SDS 2 finally decommissioned and put on a graveyard orbit.[2]
References
See also