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Configuration Overview
 Microsat
spacecraft (approx. 180 lbs [81.6 kg])
- Low-cost 3-axis stabilization
- Magnetic torquers for actuation
- Magnetometer for sensor
- On-board processing for navigation)
Triple-junction solar cells
- Experimental cells for Solar Cell Measurement System
- Experimental panels for energy conversion
- Commercial, triple-junction cells to mitigate risk
Existing hardware from heritage components
Launch
via EELV (Atlas V) using ESPA
- 560 km circular, 35.4 deg inclination
- Launch in Oct., 2006
Command
ground station at NPS
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