Ho'oponopono 2
General
| Designation | 39403 / 13064Z |
| Launch date | 20 Nov 2013 |
| Country of origin | United States |
| Mission | Technology |
| Perigee/Apogee | 400 km |
| Inclination | 40.5° |
| Period | 94.5 min |
| Launch vehicle | Minotaur #15 |
Developed by students of University of Hawaii.
3U cubesat for radar calibration.
Downlink: 437.220 MHz
End of life
| Decay | 26 Aug 2021 |
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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