Dove 2
General
| Designation | 39132 / 13015C |
| Launch date | 19 Apr 2013 |
| Country of origin | United States |
| Mission | Remote sensing |
| Perigee/Apogee | 568/585 km |
| Inclination | 64.9° |
| Period | 96.1 min |
| Launch vehicle | Soyuz 2 #20 |
Transmits in S-band and X-band.
External resources
sat-index articles
Technical data
Specifications
| Prime contractor | Cosmogia |
| Platform | |
| Mass at launch | 5.8 kg |
| Dry mass | |
| Dimension | cubesat 3U: 10 x 10 x 34 cm |
| Solar array | 4 arrays |
| Stabilization | |
| DC power | |
| Design lifetime | 6 months |
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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