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 13144.14257145 .00000321 00000-0 81316-4 0 1637
2 25682 098.1942 213.9292 0001135 112.9123 247.2208 14.57120517750331
| Epoch (UTC): | 24 May 2013 03:25:18 |
| Eccentricity: | 0.0001135 |
| inclination: | 98.1942° |
| perigee height: | 701 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 213.9292° |
| argument of perigee: | 112.9123° |
| revolutions per day: | 14.57120517 |
| mean anomaly at epoch: | 247.2208° |
| orbit number at epoch: | 75033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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