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 44758C 19074AX 20057.86055625 .00002910 00000-0 19919-3 0 579
2 44758 53.0249 35.3558 0001817 62.0737 282.0150 15.05595975 14
| Epoch (UTC): | 26 February 2020 20:39:12 |
| Eccentricity: | 0.0001817 |
| inclination: | 53.0249° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 35.3558° |
| argument of perigee: | 62.0737° |
| revolutions per day: | 15.05595975 |
| mean anomaly at epoch: | 282.0150° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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