Lemur-2 42-49 |
USA |
Spacecraft nº: |
US spacecraft nº: |
Launch data:
|
|
| Prime manufacturer | |
| Platform | |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Lemur-2 42 (Greenberg) | Lemur-2 43 (Andis) | Lemur-2 44 (Monson) | Lemur-2 45 (Furiaus) | Lemur-2 46 (PeterG) | Lemur-2 47 (Dembitz) | Lemur-2 48 (Zachary) | Lemur-2 49 (ArtFischer) | |
| Norad ID | 42837 | 43838 | 43839 | 43840 | 42841 | 42842 | 42845 | |
| Int. code | 17042N | 17042P | 17042Q | 17042R | 17042S | 17042T | 17042W | 17042 |
| Earth orbit: | ||||||||
| Perigee / Apogee | 586 X 604 km | 586 X 604 km | 586 X 604 km | 586 X 604 km | 586 X 604 km | 586 X 604 km | 586 X 604 km | 586 X 604 km |
| Inclination | 97.6 deg | 97.6 deg | 97.6 deg | 97.6 deg | 97.6 deg | 97.6 deg | 97.6 deg | 97.6 deg |
| Period | min | min | min | min | min | min | min | min |
| Decay | ||||||||
| Ref.: #7(JR740) - update: 13.08.17 | Home |