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 25682U 99020A 13143.38721048 .00000401 00000-0 99072-4 0 1615
2 25682 098.1938 213.1854 0001153 112.7561 247.3759 14.57120247750226
| Epoch (UTC): | 23 May 2013 09:17:34 |
| Eccentricity: | 0.0001153 |
| inclination: | 98.1938° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 213.1854° |
| argument of perigee: | 112.7561° |
| revolutions per day: | 14.57120247 |
| mean anomaly at epoch: | 247.3759° |
| orbit number at epoch: | 75022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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