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 25431U 98048A 13140.49616771 .00000157 00000-0 48879-4 0 2518
2 25431 086.3973 157.9262 0002366 113.4636 048.8749 14.34218478772239
| Epoch (UTC): | 20 May 2013 11:54:28 |
| Eccentricity: | 0.0002366 |
| inclination: | 86.3973° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 157.9262° |
| argument of perigee: | 113.4636° |
| revolutions per day: | 14.34218478 |
| mean anomaly at epoch: | 48.8749° |
| orbit number at epoch: | 77223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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