Flock-3m 1-4 (Dove) |
USA |
Spacecraft nº: |
US spacecraft nº: |
| Designation | 17068 |
| Launch date | 31 Oct 2017 - 21:37 UT |
| Launch site | Va, 576E |
| Launch vehicle | Minotaur-C-XL-3210 |
| Mission | Technology |
| Prime manufacturer | |
| Platform | |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Flock-3m 1 | Flock-3m 2 | Flock-3m 3 | Flock-3m 4 | |
| Norad ID | 42993 | 42994 | 42995 | 42996 |
| Int. code | 17068G | 17068H | 17068J | 17068K |
| Deployment date | 1 | 2 | 3 | 4 |
| Earth orbit: | ||||
| Perigee / Apogee | 500 x 526 km | 500 x 531 km | 500 x 532 km | 500 x 523 km |
| Inclination | 97.4 deg | 97.4 deg | 97.4 deg | 97.4 deg |
| Period | min | min | min | min |
| Decay | 1 | 2 | 3 | 4 |
| Ref.: #7(JR742) - update: 04.12.17 | Home |