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 25510U 98061C 14211.79179457 .00001268 00000-0 21725-3 0 9206
2 25510 031.4355 051.8682 0333032 115.1630 341.5729 14.35756126825856
| Epoch (UTC): | 30 July 2014 19:00:11 |
| Eccentricity: | 0.0333032 |
| inclination: | 31.4355° |
| perigee height: | 534 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 51.8682° |
| argument of perigee: | 115.1630° |
| revolutions per day: | 14.35756126 |
| mean anomaly at epoch: | 341.5729° |
| orbit number at epoch: | 82585 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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