View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 27841U 03031B 11345.75947207 .13974069 21870-5 13383-3 0 9997
2 27841 096.6971 162.6198 0013606 239.9531 120.1238 16.50719992472934
| Epoch (UTC): | 11 December 2011 18:13:38 |
| Eccentricity: | 0.0013606 |
| inclination: | 96.6971° |
| perigee height: | 128 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 162.6198° |
| argument of perigee: | 239.9531° |
| revolutions per day: | 16.50719992 |
| mean anomaly at epoch: | 120.1238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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