Launch data:
| Designation | 43933 / 19003B |
| Launch date | 18 Jan 2019 - 00:50 UT |
| Launch site | Uchinoura, LP-M |
| Launch vehicle | Epsilon CLPS |
| Mission | Technology |
| Earth orbit: | |
| Perigee / Apogee | 489 x 513 km |
| Eccentricity | |
| Inclination | 97.3° |
| Period | min |
OrigamiSat-1 (FO-98, Fuji-OSCAR 98) |
Japan |
Int. spacecraft nº: |
Japanese spacecraft nº: 258 |
Launch data:
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| Prime manufacturer | Tokyo Institute of Technology |
| Platform | CubeSat 3U |
| Operator | Tokyo Institute of Technology |
| Mass at launch | 4 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | Solar cells |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR760), #14 - update: 28.04.19 | Home |