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 39685U 14022F 14133.79926973 .10230793 12532-4 76634-3 0 9995
2 39685 051.6478 260.9431 0011364 321.6786 038.9487 16.39478651 3997
| Epoch (UTC): | 13 May 2014 19:10:56 |
| Eccentricity: | 0.0011364 |
| inclination: | 51.6478° |
| perigee height: | 160 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 260.9431° |
| argument of perigee: | 321.6786° |
| revolutions per day: | 16.39478651 |
| mean anomaly at epoch: | 38.9487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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