Tansei 2
General
| Designation | 07122 / 74008A |
| Launch date | 16 Feb 1974 |
| Country of origin | Japan |
| Mission | technology |
| Perigee/Apogee | 284/3231 km |
| Inclination | 31.2° |
| Period | 121.7 min |
| Launch vehicle | Mu 3C |
| Launch site | Kagoshima |
| Mass at launch | 56 kg |
End of life
| Decay | 22 Jan 1983 |
External resources
http://www.isas.jaxa.jp/info/sat/tanseiII-e3.html
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V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly