Hodoyoshi 3 & 4
General
| Designation |
#3:
40015 / 14033F #4: 40011 / 14033B |
| Launch date | 19 Jun 2014 |
| Country of origin | Japan |
| Mission | Remote sensing |
| Perigee/Apogee | 615/670 km |
| Inclination | 98° |
| Period | 97 min |
| Launch vehicle | Dnepr #20 |
Hodoyoshi 3 has medium resolution: 40 m to 200 m
Hodoyoshi 4 has high resolution: 5 m
External resources
http://www.nestra.jp/eng/
sat-index articles
Technical data
Specifications
| Prime contractor | University of Tokyo |
| Platform | Axelspace |
| Mass at launch | 60 kg |
| Dry mass | |
| Dimension | |
| Solar array | 2 panels |
| Stabilization | 3-axis |
| DC power | 100 W |
| Design lifetime |
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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