Unisat 2
General
| Designation | 27608 / 02058D |
| Launch date | 20 Dec 2002 |
| Country of origin | Italy |
| Mission | Technology |
| Perigee/Apogee | 650 km |
| Inclination | 64.6° |
| Period | 98 min |
| Launch vehicle | Dnepr #3 |
External resources
sat-index articles
Technical data
Specifications
| Prime contractor | GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi "la Sapienza") in Roma |
| Platform | |
| Mass at launch | 12 kg |
| Mass in orbit | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |
It carries a camera and a debris detector.
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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