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 25166.86804874 .00005049 00000-0 18657-3 0 9997
2 20580 28.4692 53.8560 0002630 76.5975 283.4912 15.25313538732484
| Epoch (UTC): | 15 June 2025 20:49:59 |
| Eccentricity: | 0.0002630 |
| inclination: | 28.4692° |
| perigee height: | 488 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 53.8560° |
| argument of perigee: | 76.5975° |
| revolutions per day: | 15.25313538 |
| mean anomaly at epoch: | 283.4912° |
| orbit number at epoch: | 73248 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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