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 25260U 98017A 13140.06013727 .00000131 00000-0 80059-4 0 5442
2 25260 098.5131 196.1225 0001812 076.1210 284.0176 14.20893903785703
| Epoch (UTC): | 20 May 2013 01:26:35 |
| Eccentricity: | 0.0001812 |
| inclination: | 98.5131° |
| perigee height: | 821 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 196.1225° |
| argument of perigee: | 76.1210° |
| revolutions per day: | 14.20893903 |
| mean anomaly at epoch: | 284.0176° |
| orbit number at epoch: | 78570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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