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 39683U 14022D 14145.84363922 .08313047 12544-4 33243-3 0 9994
2 39683 051.6422 196.6006 0001982 013.0557 348.1016 16.44047317 5937
| Epoch (UTC): | 25 May 2014 20:14:50 |
| Eccentricity: | 0.0001982 |
| inclination: | 51.6422° |
| perigee height: | 154 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 196.6006° |
| argument of perigee: | 13.0557° |
| revolutions per day: | 16.44047317 |
| mean anomaly at epoch: | 348.1016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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