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 25321.64305954 .00009681 00000-0 34065-3 0 9998
2 20580 28.4683 83.2419 0001460 330.3041 29.7471 15.27574425756156
| Epoch (UTC): | 17 November 2025 15:26:00 |
| Eccentricity: | 0.0001460 |
| inclination: | 28.4683° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 83.2419° |
| argument of perigee: | 330.3041° |
| revolutions per day: | 15.27574425 |
| mean anomaly at epoch: | 29.7471° |
| orbit number at epoch: | 75615 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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