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 14206.09981026 .00000130 00000-0 12984-4 0 8344
2 15495 082.5246 098.2884 0019711 215.8142 144.1753 14.83245110593083
| Epoch (UTC): | 25 July 2014 02:23:43 |
| Eccentricity: | 0.0019711 |
| inclination: | 82.5246° |
| perigee height: | 605 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 98.2884° |
| argument of perigee: | 215.8142° |
| revolutions per day: | 14.83245110 |
| mean anomaly at epoch: | 144.1753° |
| orbit number at epoch: | 59308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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