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 14110.43375512 .00003714 00000-0 42061-3 0 2154
2 26546 064.5583 341.1437 0017293 215.6729 202.1962 14.87788746734818
| Epoch (UTC): | 20 April 2014 10:24:36 |
| Eccentricity: | 0.0017293 |
| inclination: | 64.5583° |
| perigee height: | 593 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 341.1437° |
| argument of perigee: | 215.6729° |
| revolutions per day: | 14.87788746 |
| mean anomaly at epoch: | 202.1962° |
| orbit number at epoch: | 73481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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