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 22176.57004652 .00001602 00000-0 83753-4 0 9990
2 20580 28.4696 115.0173 0002729 121.7140 47.1072 15.10605657567449
| Epoch (UTC): | 25 June 2022 13:40:52 |
| Eccentricity: | 0.0002729 |
| inclination: | 28.4696° |
| perigee height: | 532 km |
| apogee height: | 536 km |
| right ascension of ascending node: | 115.0173° |
| argument of perigee: | 121.7140° |
| revolutions per day: | 15.10605657 |
| mean anomaly at epoch: | 47.1072° |
| orbit number at epoch: | 56744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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