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Servis 1

Space Environment Reliability Verification Integrated System


Designation 28060 / 03050A
Launch date 30 Oct 2003
Country of origin Japan
Mission Technology
Perigee/Apogee 1000 km, sun-synchronous
Inclination 99.5°
Period 105 min
Launch vehicle Rokot #10

Owned by the institute for Unmanned Space Experiment Free Flyer (Japan).

Will evaluate COTS components in space environment and a lithium-ion battery.

External resources


sat-index articles

Technical data


Prime contractor Melco
Mass at launch 980 kg
Mass in orbit 850 kg
Dimension 1.4 x 1.4 x 2.3 m
Solar array  
DC power EOL: 1200 W
Design lifetime 2 years

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