CSO 2
General
| Designation | 47305 / 20104A |
| Launch date | 29 Dec 2020 |
| Country of origin | France |
| Mission | Military: Remote sensing (identification) |
| Perigee/Apogee | 480 km, sun-synchronous |
| Inclination | 97.3° |
| Period | |
| Launch vehicle | Soyuz VS25 |
same payload as CSO 1
sat-index articles
Technical data
Specifications
| Prime contractor | Airbus Defence and Space |
| Platform | Astrosat-1000 |
| Mass at launch | 3562 kg |
| Dry mass | |
| Dimension | |
| Solar array | |
| Stabilization | 3-axis |
| DC power | |
| Design lifetime | 10 years |
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V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly
V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly