Hodoyoshi 3
Japanese micro-satellite launched in 2014 / From Wikipedia, the free encyclopedia
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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.[1] For orbit-keeping, a hydrogen peroxide thruster is used. The satellite was developed under the Funding Program for World-Leading Innovation R&D on Science and Technology.[2]
Quick Facts Mission type, Operator ...
Mission type | Earth observation |
---|---|
Operator | NESTRA |
COSPAR ID | 2014-033F |
SATCAT no. | 40015 |
Website | At u-Tokyo.ac.jp |
Mission duration | 3591 days (ongoing) |
Spacecraft properties | |
Manufacturer | University of Tokyo |
Launch mass | 60 kg (130 lb) |
Start of mission | |
Launch date | 19:11, June 19, 2014 (UTC) (2014-06-19T19:11Z) |
Rocket | Dnepr |
Launch site | Dombarovsky |
Orbital parameters | |
Reference system | Geocentric |
Eccentricity | 0 |
Perigee altitude | 600 km (370 mi) |
Apogee altitude | 600 km (370 mi) |
Inclination | 97.9° |
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