QZSS 4 (Michibiki 4) |
Japan |
Int. spacecraft nº: |
Japanese spacecraft nº: 239 |
| Designation | 42965 / 17062A |
| Launch date | 09 Oct 2017 - 22:01 UT |
| Launch site | Tanegashima, YLP-1 |
| Launch vehicle | H-2A-202 |
| Mission | Navigation |
| Inclined synchronous Earth orbit: | |
| Perigee / Apogee | 35889 x 36070 km |
| Eccentricity | |
| Inclination | 40.4° |
| 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(JR742) - update: 30.11.17 | Home |