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 25104U 97082A 13140.51767896 .00000145 00000-0 44551-4 0 2903
2 25104 086.3966 157.6919 0002261 107.0386 002.6582 14.34218108806993
| Epoch (UTC): | 20 May 2013 12:25:27 |
| Eccentricity: | 0.0002261 |
| inclination: | 86.3966° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 157.6919° |
| argument of perigee: | 107.0386° |
| revolutions per day: | 14.34218108 |
| mean anomaly at epoch: | 2.6582° |
| orbit number at epoch: | 80699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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