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Mission
Profile |
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| General |
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Design
Life: |
1
year |
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Satellite mass: |
68 kg |
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Payload:
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Earth Observation
and Scientific Instruments |
| Satelital
Attitude Control |
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Accuracy |
±
2 Degrees |
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Knowledge: |
±
1.5 Degrees (Post Facto) |
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Orbit |
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Type: |
Circular Orbit |
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Altitude: |
380 km |
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Inclination: |
51.6 Degrees |
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Ground Track error |
+/- 10 km (EOL) |
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Eccentricity: |
< 0.05 |
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