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 22178.21252299 .00001642 00000-0 86091-4 0 9997
2 20580 28.4698 104.1336 0002692 138.3254 340.3249 15.10611267567695
| Epoch (UTC): | 27 June 2022 05:06:01 |
| Eccentricity: | 0.0002692 |
| inclination: | 28.4698° |
| perigee height: | 532 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 104.1336° |
| argument of perigee: | 138.3254° |
| revolutions per day: | 15.10611267 |
| mean anomaly at epoch: | 340.3249° |
| orbit number at epoch: | 56769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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