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 25544U 98067A 13145.24030940 .00012737 00000-0 22656-3 0 8731
2 25544 051.6497 222.1187 0009791 355.7461 057.2854 15.50491999831144
| Epoch (UTC): | 25 May 2013 05:46:02 |
| Eccentricity: | 0.0009791 |
| inclination: | 51.6497° |
| perigee height: | 408 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 222.1187° |
| argument of perigee: | 355.7461° |
| revolutions per day: | 15.50491999 |
| mean anomaly at epoch: | 57.2854° |
| orbit number at epoch: | 83114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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