Himawari 9 |
Japan |
Int. spacecraft nº: |
Japanese spacecraft nº: 221 |
| Designation | 41836 / 16064A |
| Launch date | 02 Nov 2016 - 06:20 UT |
| Launch site | Tanegashima, LP1 |
| Launch vehicle | H-2A-202 |
| Mission | Weather |
| Earth orbit: | |
| Perigee / Apogee | 243 x 35857 km |
| Eccentricity | |
| Inclination | 22.4 ° |
| Period | min |
| Prime manufacturer | |
| Platform | |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR732) - update: 03.02.17 | Home |