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 13139.26705640 .00000414 00000-0 10195-3 0 1495
2 25682 098.1934 209.1313 0001075 115.6188 244.5124 14.57116419749620
| Epoch (UTC): | 19 May 2013 06:24:33 |
| Eccentricity: | 0.0001075 |
| inclination: | 98.1934° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 209.1313° |
| argument of perigee: | 115.6188° |
| revolutions per day: | 14.57116419 |
| mean anomaly at epoch: | 244.5124° |
| orbit number at epoch: | 74962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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