Lemur-2 14-17 |
USA |
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 14 (Sokolsky) | Lemur-2 15 (Xiaoqing) | Lemur-2 16 (Anubhavthakur) | Lemur-2 17 (Wingo) | ||||||||
| Norad ID | 41871 | 41872 | 41873 | 41874 | |||||||
| Int. code | 16062C | 16062D | 16062E | 16062F | >|||||||
| Deployment date | 25 Nov 16 - 20:15 | 25 Nov 16 - 20:15 | 26 Nov 16 - 00:10 | 26 Nov 16 - 00:10 | |||||||
| Earth orbit: | |||||||||||
| Perigee / Apogee | 498 x 507 km | 498 x 507 km | 498 x 507 km | 498 x 507 km | |||||||
| Inclination | 51.6° | 51.6° | 51.6° | 51.6° | |||||||
| Period | min | min | min | min | |||||||
| Decay | |||||||||||
| Ref.: #7(JR732), #14 - update: 03.02.17 | Home |