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 |