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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.〔http://park.itc.u-tokyo.ac.jp/nsat/hodo3.html〕 For orbit-keeping, a hydrogen peroxide thruster is used. The latest information is available on FACEBOOK page.〔https://www.facebook.com/hodoyoshisat〕 The satellite was developed under the Funding Program for World-Leading Innovation R&D on Science and Technology.〔http://www.jsps.go.jp/english/e-first/〕 ==Launch== Hodoyoshi-3 was launched from Dombarovsky (air base) site 13, Russia, on 19 June 2014 by a Dnepr-1 rocket. Two-side communication with Earth was successfully achieved at 2nd pass over ground station.
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