| Mission type | Communications | 
|---|---|
| Operator | SBS | 
| COSPAR ID | 1980-091A[1] | 
| SATCAT no. | 12065 | 
| 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 | 15 November 1980, 22:49 UTC | 
| Rocket | Delta-3910 PAM-D | 
| Launch site | Cape Canaveral LC-17A | 
| Contractor | NASA | 
| End of mission | |
| Disposal | Decommissioned | 
| Deactivated | June 1990 | 
| Orbital parameters | |
| Reference system | Geocentric | 
| Regime | Geostationary | 
| Longitude | 149° W[2] | 
| Eccentricity | 0.7415 | 
| Perigee altitude | 600 kilometres (370 mi) | 
| Apogee altitude | 40,662 kilometres (25,266 mi) | 
| Inclination | 62.8° | 
| Period | 736.2 minutes | 
| Epoch | November 15, 1980 | 
| Transponders | |
| Band | 14 Ku band | 
SBS 1 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 149°W longitude.[3]
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.[4]
History
On November 15, 1980, SBS 1 was launched by a Delta-3910 PAM-D from Cape Canaveral at 22:49 UTC.
In June 1990, SBS 1 was finally decommissioned and put into a graveyard orbit.[3]
References
- ↑ "SBS 1". NASA Space Science Data Coordinated Archive. Retrieved 2017-04-29.
- ↑ "SBS 1". n2yo.com. Retrieved 2017-04-29.
- 1 2 Krebs, Gunter Dirk. "SBS 1, 2, 3, 4, 5 / HGS 5 - Gunter's Space Page". Gunter's Space Page. Retrieved 2017-04-29.
- ↑ "SBS 1". NASA Space Science Data Coordinated Archive. Retrieved 2017-04-29.
See also
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