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 26548U 00057D 19081.90948695 +.00000050 +00000-0 +21912-4 0 9990
2 26548 064.5507 149.8840 0038496 307.3704 052.3901 14.89293889001745
| Epoch (UTC): | 22 March 2019 21:49:39 |
| Eccentricity: | 0.0038496 |
| inclination: | 64.5507° |
| perigee height: | 573 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 149.8840° |
| argument of perigee: | 307.3704° |
| revolutions per day: | 14.89293889 |
| mean anomaly at epoch: | 52.3901° |
| orbit number at epoch: | 174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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