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 25118.90038554 .00010015 00000-0 38476-3 0 9993
2 20580 28.4697 18.8626 0001952 270.3861 89.6509 15.24721539725154
| Epoch (UTC): | 28 April 2025 21:36:33 |
| Eccentricity: | 0.0001952 |
| inclination: | 28.4697° |
| perigee height: | 490 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 18.8626° |
| argument of perigee: | 270.3861° |
| revolutions per day: | 15.24721539 |
| mean anomaly at epoch: | 89.6509° |
| orbit number at epoch: | 72515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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