Intelsat-2 1 |
INTELSAT / US |
Spacecraft n°: |
INTELSAT spacecraft n°: 2 |
Launch data:
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| Prime manufactor | Hughes |
| Platform | HS-303A |
| Operator | Intelsat |
| Mass at launch | 162 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Out of service | 26 Oct 1966 |
| Cause | Failed to achieve geosynchronous orbit due to short burn of apogee engine |