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 25345.22461499 .00013114 00000-0 45771-3 0 9997
2 20580 28.4689 282.8025 0001816 220.1397 139.9064 15.28018696759763
| Epoch (UTC): | 11 December 2025 05:23:26 |
| Eccentricity: | 0.0001816 |
| inclination: | 28.4689° |
| perigee height: | 480 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 282.8025° |
| argument of perigee: | 220.1397° |
| revolutions per day: | 15.28018696 |
| mean anomaly at epoch: | 139.9064° |
| orbit number at epoch: | 75976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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