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 39576U 14009E 14297.85867254 .09345816 76764-5 25176-3 0 9997
2 39576 064.9818 300.5833 0008491 317.3597 044.3862 16.45008906 37698
| Epoch (UTC): | 24 October 2014 20:36:29 |
| Eccentricity: | 0.0008491 |
| inclination: | 64.9818° |
| perigee height: | 147 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 300.5833° |
| argument of perigee: | 317.3597° |
| revolutions per day: | 16.45008906 |
| mean anomaly at epoch: | 44.3862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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