Flock-2p 1-12 (Dove 0Exx) |
US |
Spacecraft nº: |
US spacecraft nº: |
| Designation | 16040 (see table) |
| Launch date | 22 June 2016 - 03:55 UT |
| Launch site | Sriharikota, SLP |
| Launch vehicle | PSLV-XL |
| Mission | Technology |
| Prime manufacturer | Planet Labs |
| Platform | CubeSat (3U) |
| Operator | Planet Labs |
| Mass at launch | 5 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | Solar cells |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Flock-2p 1 | Flock-2p 2 | Flock-2p 3 | Flock-2p 4 | Flock-2p 5 | Flock-2p 6 | Flock-2p 7 | Flock-2p 8 | Flock-2p 9 | Flock-2p 10 | ||
| Norad ID | 41617 | 41609 | 41618 | 41611 | 41616 | 41606 | 41615 | 41613 | 41610 | 41612 | |
| Int. code | 16040U | 16040L | 16040V | 16040N | 16040T | 16040H | 16040S | 16040Q | 16040M | 16040P | |
| Deployment date | 7 | 8 | 9 | 10 | |||||||
| Earth orbit | |||||||||||
| Perigee / Apogee | 499x513 km | 499x514 km | 499x513 km | 499x514 km | 499x514 km | 500x514 km | 499x514 km | 499x514 km | 499x514 km | 499x514 km | |
| Inclination | 97.5 deg | 97.5 deg | 97.5 deg | 97.5 deg | 97.5 deg | 97.5 deg | 97.5 deg | 97.5 deg | 97.5 deg | 97.5 deg | |
| Period | 94.6 min | 94.6 min | 94.6 min | 94.6 min | 94.6 min | 94.6 min | 94.6 min | 94.6 min | 94.6 min | 94.6 min | |
| Decay | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | 10 | |
| Flock-2p 11 | Flock-2p 12 | ||||||||||
| Norad ID | 41608 | 41614 | |||||||||
| Int. code | 16040K | 16040R | |||||||||
| Deployment date | 11 | 12 | |||||||||
| Earth orbit | |||||||||||
| Perigee / Apogee | 499x513 km | 499x513 km | |||||||||
| Inclination | 97.5 deg | 97.5 deg | |||||||||
| Period | 94.6 min | 94.6 min | |||||||||
| Decay | 11 | 12 | |||||||||
| Ref.: #7(JR727), #14, #228 - update: 09.04.17 | Home |