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 data is extracted from the following two-line orbital elements,
1 15495U 85009B 16267.99738952 .00000134 00000-0 13147-4 0 9998
2 15495 82.5223 76.7944 0021407 125.9306 234.3900 14.83728201710493
| Epoch (UTC): | 23 September 2016 23:56:14 |
| Eccentricity: | 0.0021407 |
| inclination: | 82.5223° |
| perigee height: | 602 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 76.7944° |
| argument of perigee: | 125.9306° |
| revolutions per day: | 14.83728201 |
| mean anomaly at epoch: | 234.3900° |
| orbit number at epoch: | 71049 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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