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 14781U 84021B 15061.17583420 .00001114 00000-0 14618-3 0 9999
2 14781 097.8161 120.8298 0009895 064.9798 295.2442 14.82192814666173
| Epoch (UTC): | 02 March 2015 04:13:12 |
| Eccentricity: | 0.0009895 |
| inclination: | 97.8161° |
| perigee height: | 615 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 120.8298° |
| argument of perigee: | 64.9798° |
| revolutions per day: | 14.82192814 |
| mean anomaly at epoch: | 295.2442° |
| orbit number at epoch: | 66617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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