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 37873U 11065B 11326.62730923 .12246307 12699-4 13812-3 0 9990
2 37873 051.4209 285.7430 0016524 077.3660 283.3856 16.48859511 2204
| Epoch (UTC): | 22 November 2011 15:03:19 |
| Eccentricity: | 0.0016524 |
| inclination: | 51.4209° |
| perigee height: | 131 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 285.7430° |
| argument of perigee: | 77.3660° |
| revolutions per day: | 16.48859511 |
| mean anomaly at epoch: | 283.3856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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