GEOStar-1
The GEOStar-1 is a communications satellite spacecraft model made by Northrop Grumman Innovation Systems in the late 1990s[1] for telecommunications in geosynchronous orbit.[2] The GEOStar-1 satellite bus is designed for a 15-year mission[3] and was compatible with the Ariane 4, Ariane 5, Delta II, Proton (rocket family), and Long March (rocket family).
Satellite Orders
[edit]| Satellite | Country | Operator | Type | Coverage | Launch date (GMT) | Rocket | Changes | Status |
|---|---|---|---|---|---|---|---|---|
| BSAT-2a | Japan | BSAT Corp | Television broadcasting | 4 Ku-band | 8 March 2001 | Ariane 5G | Retired | |
| BSAT-2b | Japan | BSAT Corp | Television broadcasting | 4 Ku-band | 12 July 2001 | Ariane 5G | Partial launch failure | |
| BSAT-2c | Japan | BSAT Corp | Television broadcasting | 4 Ku-band | 11 June 2003 | Ariane 5G | Retired | |
| IndoStar-1 | Indonesia | Media Citra Indovision | Television broadcasting | 5 S-band | 12 November 1997 | Ariane 44L | Retired |
References
[edit]- ^ "GSSAP – Spacecraft & Satellites". Retrieved 2021-04-18.
- ^ "OSC: StarBus → Star-1". 27 August 2015. Retrieved 16 June 2020.
- ^ "OSC → Orbital ATK → Northrop Grumman Innovation Systems (NGIS): Aquila → GeoStar-1". space.skyrocket.de. Retrieved 2021-04-18.
 | This spacecraft or satellite related article is a stub. You can help Wikipedia by expanding it. |