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 25778U 99032B 13170.42736677 .00000226 00000-0 73645-4 0 2831
2 25778 086.3988 113.7396 0002658 129.9998 019.7708 14.34220026739028
| Epoch (UTC): | 19 June 2013 10:15:24 |
| Eccentricity: | 0.0002658 |
| inclination: | 86.3988° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 113.7396° |
| argument of perigee: | 129.9998° |
| revolutions per day: | 14.34220026 |
| mean anomaly at epoch: | 19.7708° |
| orbit number at epoch: | 73902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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