Optsat 3000
General
| Designation | 42900 / 17044A |
| Launch date | 2 Aug 2017 |
| Country of origin | Italy |
| Mission | Remote sensing |
| Perigee/Apogee | 450 km, sun-synchronous |
| Inclination | 97.2° |
| Period | 93.6 min |
| Launch vehicle | Vega #10 |
Italian military optical remote sensing. Launch initially planned in 2015.
The camera is worth $40 million, built by Elop
sat-index articles
Technical data
Specifications
| Prime contractor | Telespazio & IAI |
| Platform | Optsat 3000 |
| Mass at launch | 368 kg |
| Dry mass | |
| Dimension | |
| Solar array | |
| Stabilization | 3-axis |
| DC power | |
| Design lifetime | 7 years |
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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