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 20580U 90037B 22139.30327672 .00004206 00000-0 23836-3 0 9998
2 20580 28.4714 1.9427 0002867 80.2160 71.2576 15.10459505561809
| Epoch (UTC): | 19 May 2022 07:16:43 |
| Eccentricity: | 0.0002867 |
| inclination: | 28.4714° |
| perigee height: | 533 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 1.9427° |
| argument of perigee: | 80.2160° |
| revolutions per day: | 15.10459505 |
| mean anomaly at epoch: | 71.2576° |
| orbit number at epoch: | 56180 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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