ZY-1 02D (Zi Yuan-1 02D) |
China |
Int. spacecraft nº: |
Chinese spacecraft nº: 489 |
| Designation | 44528 / 19059A |
| Launch date | 12 Sep 2019 - 03:26 UTC |
| Launch site | Taiyuan, LC-9 |
| Launch vehicle | CZ-4B |
| Mission | Imaging |
| Earth orbit: | |
| Perigee / Apogee | 780 x 781 km |
| Eccentricity | |
| Inclination | 98.6° |
| Period | 100.3 min |
| Prime manufacturer | |
| Platform | |
| Operator | |
| Mass at launch | 1840 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR770), #27, #228 - update: 13.11.19 | Home |