Quakesat

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General

Designation	27845 / 03031F
Launch date	30 Jun 2003
Country of origin	United States
Mission
Perigee/Apogee	820 km, sunsynchronous
Inclination
Period
Launch vehicle	Rokot #9

Operated by Stanford University and Quakesat LLC. To detect ELF radio emission of sismic activity.

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External resources

http://www.quakefinder.com/quakesat.htm

sat-index articles

Technical data

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Specifications

Prime contractor
Platform
Mass at launch	3 kg
Mass in orbit
Dimension
Solar array
Stabilization
DC power
Design lifetime

Downlink: 436.675 MHz

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