Xiaoxiang-1 02 xing (TY1-02) |
China |
Int. spacecraft nº: |
Chinese spacecraft nº: 423 |
| Designation | 43664 / 18083C |
| Launch date | 29 Oct 2018 - 00:43 UT |
| Launch site | Jiuquan, SLS-2 |
| Launch vehicle | CZ-2C |
| Mission | Technology |
| Earth orbit: | |
| Perigee / Apogee | 509 x 522 km |
| Eccentricity | |
| Inclination | 97.52° |
| Period | min |
| Prime manufacturer | Tiangyi Research Institute |
| Platform | 6U Cubesat |
| Operator | LFLT |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | laser communications payload |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR756), #22 - update: 07.11.18 | Home |