Kinshachi 2 (ChubuSat 2) |
Japan |
Spacecraft nº: |
Japanese spacecraft nº: 216 |
Designation | 41338 / 16012B |
Launch date | 17 Feb 2016 - 08:45 UT |
Launch site | Tanegashima, YLP-1 |
Launch vehicle | H-2A-202 |
Mission | Civil: Technology, Space Science |
LEO Sun-Synchronous Earth orbit: | |
Perigee / Apogee | 559 x 579 km |
Eccentricity | 1,37E-03 |
Inclination | 31.0 ° |
Period | 96.05 min |
Prime manufacturer | Nagoya University and Daido University |
Platform | |
Operator | Nagoya University and Daido University |
Mass at launch | 50 kg |
Dry Mass | kg |
Basic shape | |
Dimension (m) | |
Equipment | |
Solar array | |
Stabilization | |
Propulsion | |
DC power | |
Uplink (MHz) | 145.815 |
Downlink (MHz) | 437.100 |
Beacon (MHz) | 437.102 |
Mode | 1k2 AFSK 9k6 GMSK CW |
Call sign | JJ2YPN |
Status | Inactive |
Design lifetime |
Ref.: #7(JR723), #226, #228 - update: 15.04.17 | Home |