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 24276.43585777 .00017177 00000-0 76904-3 0 9993
2 20580 28.4698 345.5748 0003284 129.5775 230.5108 15.19839067693357
| Epoch (UTC): | 02 October 2024 10:27:38 |
| Eccentricity: | 0.0003284 |
| inclination: | 28.4698° |
| perigee height: | 504 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 345.5748° |
| argument of perigee: | 129.5775° |
| revolutions per day: | 15.19839067 |
| mean anomaly at epoch: | 230.5108° |
| orbit number at epoch: | 69335 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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