Designation | 26575 / 00065A |
Launch date | 20 Oct 2000 |
Country of origin | United States |
Mission | Military: Telecommunications |
Geostationary orbit | unofficial: 12°W |
Launch vehicle | Atlas Centaur #130 |
Prime contractor | Lockheed Martin |
Platform | |
Mass at launch | 1168 kg |
Dry mass | approx 900 kg |
Dimension | |
Solar array | |
Stabilization | 3-axis |
DC power | 1700 W |
Design lifetime |