Lemur-2 68-71 |
USA |
Spacecraft nº: |
US spacecraft nº: |
Launch data:
|
|
| Prime manufacturer | SpireGlobal |
| Platform | Cubesat (3U) |
| Operator | SpireGlobal |
| Mass at launch | 4 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | GNSS-RO meteorology payloads. |
| Solar array | Solar cells |
| Stabilization | |
| Propulsion | None |
| DC power | |
| Design lifetime |
| Lemur-2 68 | Lemur-2 69 | Lemur-2 70 | Lemur-2 71 | |
| Name | PeterWebster | DaveWilson | MCCafferty | BrownCow |
| Norad ID | 43124 | 43126 | 43123 | 43125 |
| Int. code | 18004P | 18004R | 18004N | 18004Q |
| Earth orbit: | ||||
| Perigee / Apogee | 495 x 508 | |||
| Inclination | 97.6deg | |||
| Period | 94.6 min | |||
| Decay | ||||
| Ref.: #7(JR745), #228 - update: 21.01.18 | Home |