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 24284.56054521 .00018604 00000-0 66185-3 0 9996
2 53807 53.2351 20.9848 0008966 85.3634 274.8391 15.29008253115863
Epoch (UTC): | 10 October 2024 13:27:11 |
Eccentricity: | 0.0008966 |
inclination: | 53.2351° |
perigee height: | 472 km |
apogee height: | 485 km |
right ascension of ascending node: | 20.9848° |
argument of perigee: | 85.3634° |
revolutions per day: | 15.29008253 |
mean anomaly at epoch: | 274.8391° |
orbit number at epoch: | 11586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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