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 24252.91229736 .00018243 00000-0 66987-3 0 9991
2 53807 53.2346 167.3416 0007767 5.5444 354.5642 15.27990722111023
Epoch (UTC): | 08 September 2024 21:53:42 |
Eccentricity: | 0.0007767 |
inclination: | 53.2346° |
perigee height: | 476 km |
apogee height: | 487 km |
right ascension of ascending node: | 167.3416° |
argument of perigee: | 5.5444° |
revolutions per day: | 15.27990722 |
mean anomaly at epoch: | 354.5642° |
orbit number at epoch: | 11102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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