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 25108U 97082E 13139.57343748 .00000183 00000-0 58314-4 0 2956
2 25108 086.3966 158.0834 0002336 108.5077 038.0687 14.34221793806863
| Epoch (UTC): | 19 May 2013 13:45:44 |
| Eccentricity: | 0.0002336 |
| inclination: | 86.3966° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 158.0834° |
| argument of perigee: | 108.5077° |
| revolutions per day: | 14.34221793 |
| mean anomaly at epoch: | 38.0687° |
| orbit number at epoch: | 80686 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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