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 24286.15320224 .00018111 00000-0 80312-3 0 9994
2 20580 28.4686 280.2439 0002703 229.5338 130.5020 15.20183039695095
| Epoch (UTC): | 12 October 2024 03:40:36 |
| Eccentricity: | 0.0002703 |
| inclination: | 28.4686° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 280.2439° |
| argument of perigee: | 229.5338° |
| revolutions per day: | 15.20183039 |
| mean anomaly at epoch: | 130.5020° |
| orbit number at epoch: | 69509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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