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 14114.65761718 .00001540 00000-0 16723-3 0 2206
2 26546 064.5579 327.9854 0017108 214.9467 145.1023 14.87815747735440
| Epoch (UTC): | 24 April 2014 15:46:58 |
| Eccentricity: | 0.0017108 |
| inclination: | 64.5579° |
| perigee height: | 593 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 327.9854° |
| argument of perigee: | 214.9467° |
| revolutions per day: | 14.87815747 |
| mean anomaly at epoch: | 145.1023° |
| orbit number at epoch: | 73544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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