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 25276U 98019E 13145.48514853 .00000296 00000-0 98691-4 0 3371
2 25276 086.3978 187.1773 0002371 108.2004 251.9450 14.34220478793401
| Epoch (UTC): | 25 May 2013 11:38:36 |
| Eccentricity: | 0.0002371 |
| inclination: | 86.3978° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 187.1773° |
| argument of perigee: | 108.2004° |
| revolutions per day: | 14.34220478 |
| mean anomaly at epoch: | 251.9450° |
| orbit number at epoch: | 79340 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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