Dove 2 |
USA |
Spacecraft nº: |
US spacecraft nº: |
| Designation | 39132 / 13015C |
| Launch date | 19 April 2013 - 10:00 UT |
| Launch site | Baik, LC-31/6 |
| Launch vehicle | Soyuz-2-1A |
| Mission | Technology |
| Earth orbit: | |
| Perigee / Apogee | 574 x 577 km |
| Eccentricity | |
| Inclination | 64.9 deg |
| Period | 96.0 min |
| Prime manufacturer | Cosmogia Inc. |
| Platform | CubeSat (3U) |
| Operator | Cosmogia Inc. |
| Mass at launch | 5.5 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | Solar cells |
| Stabilization | |
| Propulsion | none |
| DC power | |
| Design lifetime | ~180 days |
| Ref.: #14, #228 - update: 19.09.13 | Home |