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 37252U 10066J 10355.60473544 .12256881 92310-6 19975-2 0 9996
2 37252 034.5327 088.4640 0011338 010.1315 351.3122 16.32165367 2078
| Epoch (UTC): | 21 December 2010 14:30:49 |
| Eccentricity: | 0.0011338 |
| inclination: | 34.5327° |
| perigee height: | 179 km |
| apogee height: | 194 km |
| right ascension of ascending node: | 88.4640° |
| argument of perigee: | 10.1315° |
| revolutions per day: | 16.32165367 |
| mean anomaly at epoch: | 351.3122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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