EOS-AM 1 |
USA |
Spacecraft n°: |
USA satellite n°: |
Launch data:
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| Prime contractor | Lockheed Martin |
| Platform | |
| Mass at launch | 4854 kg |
| Mass in orbit | |
| Paylaod mass | 1100 kg |
| Dimension | |
| Solar array | |
| Stabilization | 3-axis |
| DC power | 7500 W |
| Design lifetime | 6 years |
| Ref.: #15 - update: 16.03.09 | Home |