Hodoyoshi 3
| Use attributes for filter ! | |
| Inclination | 97. 9° |
|---|---|
| Launch date | June 19, 2014 |
| Manufacturers | The University of Tokyo |
| SATCAT no. | 40015 |
| Rocket | Dnepr |
| Launch site | Yasny Launch Base |
| Date of Reg. | |
| Date of Upd. | |
| ID | 2119278 |
About Hodoyoshi 3
Hodoyoshi-3 is a Japanese micro-satellite launched in 2014. The satellite is built in 0. 5x0. 5x0. 65m box-shape bus, optimized for piggy-back launch. All instruments are powered by solar cells mounted on the spacecraft body and two stub wings, with estimated electrical power of 50W.
