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 23332.14483993 .00007972 00000-0 40559-3 0 9999
2 20580 28.4690 255.7743 0002623 358.0603 133.3186 15.15006931646593
| Epoch (UTC): | 28 November 2023 03:28:34 |
| Eccentricity: | 0.0002623 |
| inclination: | 28.4690° |
| perigee height: | 519 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 255.7743° |
| argument of perigee: | 358.0603° |
| revolutions per day: | 15.15006931 |
| mean anomaly at epoch: | 133.3186° |
| orbit number at epoch: | 64659 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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