Lemur-2 1-4 (Joel, Peter, Jeroun, Chris) |
US |
Spacecraft nº: |
US spacecraft nº: |
Launch data:
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| 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 1 (Joel) | Lemur-2 2 (Peter) | Lemur-2 3 (Jeroen) | Lemur-2 4 (Chris) | |
| Norad ID | 40933 | 40934 | 40935 | 40936 |
| Int. code | 15052D | 15052E | 15052F | 15052G |
| Earth orbit | ||||
| Perigee / Apogee | 629x650 km | 634x650 km | 635x650 km | 635x650 km |
| Inclination | 6.0 deg | 6.0 deg | 6.0 deg | 6.0 deg |
| Period | min | min | min | min |
| Decay | ||||
| Ref.: #7(JR716), #228 - update: 09.02.17 | Home |