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 18115.94787892 .00000069 00000-0 53924-5 0 9999
2 15495 82.5241 254.4928 0020657 22.5267 337.6850 14.83807879796342
| Epoch (UTC): | 25 April 2018 22:44:56 |
| Eccentricity: | 0.0020657 |
| inclination: | 82.5241° |
| perigee height: | 603 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 254.4928° |
| argument of perigee: | 22.5267° |
| revolutions per day: | 14.83807879 |
| mean anomaly at epoch: | 337.6850° |
| orbit number at epoch: | 79634 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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