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 24262.90725159 .00009267 00000-0 41496-3 0 9999
2 20580 28.4677 76.4812 0002905 358.7928 1.2658 15.19523172691551
| Epoch (UTC): | 18 September 2024 21:46:26 |
| Eccentricity: | 0.0002905 |
| inclination: | 28.4677° |
| perigee height: | 505 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 76.4812° |
| argument of perigee: | 358.7928° |
| revolutions per day: | 15.19523172 |
| mean anomaly at epoch: | 1.2658° |
| orbit number at epoch: | 69155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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