Servis 2

Space Environment Reliability Verification Integrated System

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General

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.

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External resources

http://www.usef.or.jp/english/f3_project/servis/f3_servis.html

sat-index articles

n2yo.com tracking

Technical data

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Specifications

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

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