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 29157U 06019A 11362.09373240 .21317118 -26900-6 22182-3 0 9997
2 29157 078.8598 273.8863 0005562 266.0949 094.8423 16.50817633316260
| Epoch (UTC): | 28 December 2011 02:14:58 |
| Eccentricity: | 0.0005562 |
| inclination: | 78.8598° |
| perigee height: | 133 km |
| apogee height: | 141 km |
| right ascension of ascending node: | 273.8863° |
| argument of perigee: | 266.0949° |
| revolutions per day: | 16.50817633 |
| mean anomaly at epoch: | 94.8423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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