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 39682U 14022C 14147.96574206 .06398515 12616-4 29571-3 0 9997
2 39682 051.6117 185.1924 0010905 007.8432 355.5562 16.42301551 6252
| Epoch (UTC): | 27 May 2014 23:10:40 |
| Eccentricity: | 0.0010905 |
| inclination: | 51.6117° |
| perigee height: | 152 km |
| apogee height: | 167 km |
| right ascension of ascending node: | 185.1924° |
| argument of perigee: | 7.8432° |
| revolutions per day: | 16.42301551 |
| mean anomaly at epoch: | 355.5562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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