Intelsat-4A 2 |
INTELSAT / US |
Spacecraft n°: |
INTELSAT spacecraft n°: 23 |
| Designation: | 08620 / 76010A |
| Launch date | 30 Jan 1976 |
| Launch site | CC, LC-36B |
| Launch vehicle: | Atlas-SLV3D Centaur-D1AR (AC-37) |
| Mission: | Telecommunications |
| Geostationary orbit on: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | deg |
| Period | min |
| Location | 27.5°W |
| Prime manufacturer | Hughes |
| Platform | |
| Operator | Intelsat |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Out of service | yes - Retired |