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 24260.87118105 .00011485 00000-0 51701-3 0 9995
2 20580 28.4679 90.1613 0002735 335.8657 24.1808 15.19479398690988
| Epoch (UTC): | 16 September 2024 20:54:30 |
| Eccentricity: | 0.0002735 |
| inclination: | 28.4679° |
| perigee height: | 505 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 90.1613° |
| argument of perigee: | 335.8657° |
| revolutions per day: | 15.19479398 |
| mean anomaly at epoch: | 24.1808° |
| orbit number at epoch: | 69098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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