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 39681U 14022B 14154.46327779 .09117285 12564-4 29119-3 0 9996
2 39681 051.6203 150.5796 0001470 008.4241 352.1352 16.45052853 7311
| Epoch (UTC): | 03 June 2014 11:07:07 |
| Eccentricity: | 0.0001470 |
| inclination: | 51.6203° |
| perigee height: | 151 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 150.5796° |
| argument of perigee: | 8.4241° |
| revolutions per day: | 16.45052853 |
| mean anomaly at epoch: | 352.1352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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