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 26546U 00057B 14066.20314091 .00002481 00000-0 28821-3 0 1724
2 26546 064.5567 118.9523 0021946 218.6106 213.3669 14.87505941728239
| Epoch (UTC): | 07 March 2014 04:52:31 |
| Eccentricity: | 0.0021946 |
| inclination: | 64.5567° |
| perigee height: | 590 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 118.9523° |
| argument of perigee: | 218.6106° |
| revolutions per day: | 14.87505941 |
| mean anomaly at epoch: | 213.3669° |
| orbit number at epoch: | 72823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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