Saudisat 2
General
| Designation | 28371 / 04025F |
| Launch date | 29 Jun 2004 |
| Country of origin | Saudi Arabia |
| Mission | Telecommunications |
| Perigee/Apogee | 700 km |
| Inclination | 98.3° |
| Period | 99 min |
| Launch vehicle | Dnepr #4 |
sat-index articles
Technical data
Specifications
| Prime contractor | |
| Platform | |
| Mass at launch | 35 kg |
| Mass in orbit | |
| Dimension | 29.5 x 29.5 x 50.0 cm |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |
Has a remote sensing payload with 15 m resolution.
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V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly