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 23084.15224523 .00007492 00000-0 40901-3 0 9994
2 20580 28.4691 106.8555 0002798 185.9910 226.2099 15.12475207608981
| Epoch (UTC): | 25 March 2023 03:39:13 |
| Eccentricity: | 0.0002798 |
| inclination: | 28.4691° |
| perigee height: | 527 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 106.8555° |
| argument of perigee: | 185.9910° |
| revolutions per day: | 15.12475207 |
| mean anomaly at epoch: | 226.2099° |
| orbit number at epoch: | 60898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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