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 25316.74302545 .00012631 00000-0 44825-3 0 9990
2 20580 28.4675 116.5719 0001370 260.9920 99.0520 15.27460761755403
| Epoch (UTC): | 12 November 2025 17:49:57 |
| Eccentricity: | 0.0001370 |
| inclination: | 28.4675° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.5719° |
| argument of perigee: | 260.9920° |
| revolutions per day: | 15.27460761 |
| mean anomaly at epoch: | 99.0520° |
| orbit number at epoch: | 75540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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