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 13143.11253401 .00000425 00000-0 10427-3 0 1600
2 25682 098.1937 212.9153 0001130 110.9019 249.2312 14.57120146750186
| Epoch (UTC): | 23 May 2013 02:42:02 |
| Eccentricity: | 0.0001130 |
| inclination: | 98.1937° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 212.9153° |
| argument of perigee: | 110.9019° |
| revolutions per day: | 14.57120146 |
| mean anomaly at epoch: | 249.2312° |
| orbit number at epoch: | 75018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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