AUTcube-2 |
Japan |
Int. spacecraft nº: |
Japannese spacecraft nº: 254 |
| Designation | 43679 / 18084J |
| Launch date | 29 Oct 2018 - 04:08 UT |
| Launch site | Tanegashima, YLP-1 |
| Launch vehicle | H-2A-202 |
| Mission | Technology |
| Earth orbit: | |
| Perigee / Apogee | 586 x 608 km |
| Eccentricity | |
| Inclination | 97.83° |
| Period | min |
| Prime manufacturer | Aichi University of Technology |
| Platform | 1U cubesat |
| Operator | AUT |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR756) - update: 07.11.18 | Home |