Xiaoxiang 1-08 (TY 1-08, Dianfeng) |
China |
Int. spacecraft nº: |
Chinese spacecraft nº: 504 |
| Designation | 44706 / 19072D |
| Launch date | 03 Nov 2019 - 03:22 UT |
| Launch site | TY, LC-9 |
| Launch vehicle | CZ-4B |
| Mission | Remote sensing, Imaging |
| Earth orbit: | |
| Perigee / Apogee | 492 x 512 km |
| Eccentricity | |
| Inclination | 97.5° |
| Period | 94.5 min |
| Prime manufacturer | Tianyi Research |
| Platform | 6U Cubesat |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR771), #228 - update: 20.11.19 | Home |