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 23027.32314157 .00004863 00000-0 26724-3 0 9999
2 20580 28.4699 124.3027 0001981 301.3296 104.3567 15.11770724600116
| Epoch (UTC): | 27 January 2023 07:45:19 |
| Eccentricity: | 0.0001981 |
| inclination: | 28.4699° |
| perigee height: | 529 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 124.3027° |
| argument of perigee: | 301.3296° |
| revolutions per day: | 15.11770724 |
| mean anomaly at epoch: | 104.3567° |
| orbit number at epoch: | 60011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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