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 |