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Servis 2

Space Environment Reliability Verification Integrated System


Designation 36588 / 10023A
Launch date 2 Jun 2010
Country of origin Japan
Mission Technology
Perigee/Apogee 1200 km, sun-synchronous
Inclination 100.4°
Period 109 min
Launch vehicle Rokot #18

Owned by the institute for Unmanned Space Experiment Free Flyer, Japan, sponsored by Japan's New Energy and Industrial Technology Development Organisation (NEDO) and the Ministry of Economy, Trade and Industry (METI).

Will be employed to verify the use of commercial off-the-shelf (COTS) components and technologies in space conditions.

External resources


sat-index articles

n2yo.com tracking

Technical data


Prime contractor Melco
Mass at launch 880 kg
Mass in orbit 740 kg
Dimension 1.4 x 1.4 x 2.3 m
Solar array  
DC power EOL: 1200 W
Design lifetime 1 years

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