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 14108.81883040 .00000614 00000-0 72094-4 0 7470
2 15495 082.5265 189.3146 0020918 176.7977 183.3376 14.83184240578668
| Epoch (UTC): | 18 April 2014 19:39:06 |
| Eccentricity: | 0.0020918 |
| inclination: | 82.5265° |
| perigee height: | 604 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 189.3146° |
| argument of perigee: | 176.7977° |
| revolutions per day: | 14.83184240 |
| mean anomaly at epoch: | 183.3376° |
| orbit number at epoch: | 57866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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