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 40246U 14057A 14268.84278341 -.00003690 11668-4 00000+0 0 9995
2 40246 052.0554 320.6198 0119978 105.0721 255.6490 16.09308761 01
| Epoch (UTC): | 25 September 2014 20:13:36 |
| Eccentricity: | 0.0119978 |
| inclination: | 52.0554° |
| perigee height: | 169 km |
| apogee height: | 328 km |
| right ascension of ascending node: | 320.6198° |
| argument of perigee: | 105.0721° |
| revolutions per day: | 16.09308761 |
| mean anomaly at epoch: | 255.6490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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