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 15064.51488280 .00002460 00000-0 27492-3 0 9996
2 26546 064.5554 065.8812 0020975 323.7616 036.2071 14.89130739782297
| Epoch (UTC): | 05 March 2015 12:21:25 |
| Eccentricity: | 0.0020975 |
| inclination: | 64.5554° |
| perigee height: | 586 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 65.8812° |
| argument of perigee: | 323.7616° |
| revolutions per day: | 14.89130739 |
| mean anomaly at epoch: | 36.2071° |
| orbit number at epoch: | 78229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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