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 13146.21553197 .00011523 00000-0 20563-3 0 8808
2 25544 051.6499 217.2850 0009742 358.6968 101.4114 15.50510604831290
| Epoch (UTC): | 26 May 2013 05:10:21 |
| Eccentricity: | 0.0009742 |
| inclination: | 51.6499° |
| perigee height: | 408 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 217.2850° |
| argument of perigee: | 358.6968° |
| revolutions per day: | 15.50510604 |
| mean anomaly at epoch: | 101.4114° |
| orbit number at epoch: | 83129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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