Ryusei
Also called OREX (Orbital Re-entry Experiment vehicle)
General
| Designation | 22978 / 94007A |
| Launch date | 3 Feb 1994 |
| Country of origin | Japan |
| Operator | NASDA |
| Mission | Technology |
| Perigee/Apogee | 457/449 km |
| Inclination | 30.5° |
| Period | 93.5 min |
| Launch vehicle | H2 |
End of life
| Decay | 5 Feb 1994 in the Pacific |
External resources
sat-index articles
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V0.143 - Converted on Sun, 03 Dec 2023 15:12:44 GMT - Updated quarterly
V0.143 - Converted on Sun, 03 Dec 2023 15:12:44 GMT - Updated quarterly