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 25312.62670398 .00009804 00000-0 34712-3 0 9999
2 20580 28.4659 144.5654 0001507 200.4727 159.5808 15.27381835754774
| Epoch (UTC): | 08 November 2025 15:02:27 |
| Eccentricity: | 0.0001507 |
| inclination: | 28.4659° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 144.5654° |
| argument of perigee: | 200.4727° |
| revolutions per day: | 15.27381835 |
| mean anomaly at epoch: | 159.5808° |
| orbit number at epoch: | 75477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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