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 25170U 98010B 13140.41833300 .00000390 00000-0 13203-3 0 8469
2 25170 086.3982 252.6594 0002273 108.4898 319.3991 14.34219968798374
| Epoch (UTC): | 20 May 2013 10:02:23 |
| Eccentricity: | 0.0002273 |
| inclination: | 86.3982° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 252.6594° |
| argument of perigee: | 108.4898° |
| revolutions per day: | 14.34219968 |
| mean anomaly at epoch: | 319.3991° |
| 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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