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 25073.78789295 .00013234 00000-0 52759-3 0 9990
2 20580 28.4685 324.1477 0002156 108.2909 251.7920 15.23649670718523
| Epoch (UTC): | 14 March 2025 18:54:33 |
| Eccentricity: | 0.0002156 |
| inclination: | 28.4685° |
| perigee height: | 493 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 324.1477° |
| argument of perigee: | 108.2909° |
| revolutions per day: | 15.23649670 |
| mean anomaly at epoch: | 251.7920° |
| orbit number at epoch: | 71852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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