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 13144.86362131 .00012981 00000-0 23081-3 0 8710
2 25544 051.6496 223.9863 0009650 354.2913 114.7799 15.50483599831080
| Epoch (UTC): | 24 May 2013 20:43:36 |
| Eccentricity: | 0.0009650 |
| inclination: | 51.6496° |
| perigee height: | 409 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 223.9863° |
| argument of perigee: | 354.2913° |
| revolutions per day: | 15.50483599 |
| mean anomaly at epoch: | 114.7799° |
| orbit number at epoch: | 83108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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