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 25108U 97082E 13142.50678442 .00000007 00000-0 -45551-5 0 2984
2 25108 086.3968 156.8580 0002371 108.7644 053.6520 14.34218480807285
| Epoch (UTC): | 22 May 2013 12:09:46 |
| Eccentricity: | 0.0002371 |
| inclination: | 86.3968° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 156.8580° |
| argument of perigee: | 108.7644° |
| revolutions per day: | 14.34218480 |
| mean anomaly at epoch: | 53.6520° |
| orbit number at epoch: | 80728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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