RapidEye 2 |
Germany |
Spacecraft nº: |
German spacecraft nº: 54 |
| Designation | 33312 / 08040A |
| Launch date | 29 Aug 2008 - 07:16 UT |
| Launch site | B, LC-109/95 |
| Launch vehicle | Dnepr-1 |
| Mission | Imaging |
| Earth orbit: | |
| Perigee / Apogee | 628 x 645 km |
| Eccentricity | |
| Inclination | 97.9 deg |
| Period | 97.3 min |
| Prime contractor | Surrey Satellite in Guildford |
| Operator | RapidEye AG of Brandenberg |
| Platform | |
| Mass at launch | 152 kg including 12 kg propellant |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |