Ten-Koh |
Japan |
Int. spacecraft nº: |
Japanese spacecraft nº: 252 |
| Designation | 43671 / 18084A |
| Launch date | 29 Oct 2018 - 04:08 UT |
| Launch site | Tanegashima, YLP-1 |
| Launch vehicle | H-2A-202 |
| Mission | Technology, Observation |
| Earth orbit: | |
| Perigee / Apogee | 595 x 614 km |
| Eccentricity | |
| Inclination | 97.85° |
| Period | min |
| Prime manufacturer | Kyushu Institute of Technology |
| Platform | |
| Operator | KYUT |
| Mass at launch | kg |
| Dry Mass | 22 kg |
| Basic shape | polyhedron |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR756) - update: 07.11.18 | Home |