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 25520U 98064B 13140.82114039 .00003204 00000-0 13123-3 0 2522
2 25520 028.4598 356.3830 0004831 120.3006 333.0571 15.21082904806792
| Epoch (UTC): | 20 May 2013 19:42:26 |
| Eccentricity: | 0.0004831 |
| inclination: | 28.4598° |
| perigee height: | 499 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 356.3830° |
| argument of perigee: | 120.3006° |
| revolutions per day: | 15.21082904 |
| mean anomaly at epoch: | 333.0571° |
| orbit number at epoch: | 80679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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