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 25172U 98010D 13140.41169600 .00000382 00000-0 12926-3 0 3317
2 25172 086.3979 252.5594 0002246 109.2751 317.0751 14.34220820798376
| Epoch (UTC): | 20 May 2013 09:52:50 |
| Eccentricity: | 0.0002246 |
| inclination: | 86.3979° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 252.5594° |
| argument of perigee: | 109.2751° |
| revolutions per day: | 14.34220820 |
| mean anomaly at epoch: | 317.0751° |
| orbit number at epoch: | 79837 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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