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 25285U 98021A 13169.37721523 .00000232 00000-0 75631-4 0 3382
2 25285 086.3986 114.1279 0002421 101.5875 258.5592 14.34218829795789
| Epoch (UTC): | 18 June 2013 09:03:11 |
| Eccentricity: | 0.0002421 |
| inclination: | 86.3986° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 114.1279° |
| argument of perigee: | 101.5875° |
| revolutions per day: | 14.34218829 |
| mean anomaly at epoch: | 258.5592° |
| orbit number at epoch: | 79578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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