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 21104.46611060 .00000488 00000-0 18593-4 0 9996
2 20580 28.4690 128.4543 0002944 93.8192 53.9615 15.09610226501382
| Epoch (UTC): | 14 April 2021 11:11:11 |
| Eccentricity: | 0.0002944 |
| inclination: | 28.4690° |
| perigee height: | 535 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 128.4543° |
| argument of perigee: | 93.8192° |
| revolutions per day: | 15.09610226 |
| mean anomaly at epoch: | 53.9615° |
| orbit number at epoch: | 50138 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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