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 53807U 22111AL 23080.39989938 .00004035 00000-0 19979-3 0 9991
2 53807 53.2012 114.6332 0013365 137.7140 222.4890 15.19950661 29099
| Epoch (UTC): | 21 March 2023 09:35:51 |
| Eccentricity: | 0.0013365 |
| inclination: | 53.2012° |
| perigee height: | 497 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 114.6332° |
| argument of perigee: | 137.7140° |
| revolutions per day: | 15.19950661 |
| mean anomaly at epoch: | 222.4890° |
| orbit number at epoch: | 2909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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