Star One C12
It has been suggested that AMC-12 (satellite) be merged into this article. (Discuss) Proposed since August 2021. |
Names | NSS-10 Worldsat 2 GE-1I Astra 4A AMC-12 |
---|---|
Mission type | Communications |
Operator | SES |
COSPAR ID | 2005-003A |
SATCAT no. | 28526 |
Mission duration | 16 years (planned) |
Spacecraft properties | |
Bus | Spacebus 4000C3 |
Manufacturer | Alcatel Alenia Space |
Launch mass | 4,953 kg (10,919 lb) |
Dry mass | 2,286 kg (5,040 lb) |
Start of mission | |
Launch date | 3 February 2005, 03:27 UTC |
Rocket | Proton-M / Briz-M |
Launch site | Baikonur, Site 81/24 |
Contractor | Khrunichev State Research and Production Space Center |
Entered service | 2005 |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Geostationary orbit |
Longitude | 37.5° West |
Transponders | |
Band | 72 C-band |
Star One C12 (also called as NSS-10, Worldsat 2, GE-1I, Astra 4A, and AMC-12) is a communications satellite operated by SES S.A. with headquarters in Luxembourg. It was built by Alcatel Alenia Space based on the Spacebus 4000C3 satellite bus, and was launched on 3 February 2005, at 03:27 UTC by a Proton-M launch vehicle.[1]
The mass was 4953 kg.
See also[]
References[]
- ^ {{cite web|url=http://space.skyrocket.de/doc_sdat/amc-12.htm AMC 12 / Astra 4A / Star One C12 / NSS 10|publisher=Gunter's Space Page|date=|access-date=
External links[]
Categories:
- Spacecraft launched in 2005
- Star One satellites
- Communications satellite stubs
- Brazil science stubs