General
Design Life:
3 year
Satellite mass:
190 kg
Payload:
Sun Observation and Cosmic Radiation Instruments
Spacecraft Attitude Control
Accuracy
± 3 Degrees
Knowledge:
± 2 Degrees (Post Facto)
Spacecraft Power
260 W (BOL)
Orbit
Type:
Circular Orbit
Altitude:
560 km (stable for lifetime)
Inclination:
38 Degrees
Ground Track error
+/- 10 km (EOL)
Eccentricity:
< 0.05
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