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 24252.06196806 .00019997 00000-0 73354-3 0 9991
2 53807 53.2344 171.2706 0007725 2.8215 357.2827 15.27961510110899
Epoch (UTC): | 08 September 2024 01:29:14 |
Eccentricity: | 0.0007725 |
inclination: | 53.2344° |
perigee height: | 476 km |
apogee height: | 487 km |
right ascension of ascending node: | 171.2706° |
argument of perigee: | 2.8215° |
revolutions per day: | 15.27961510 |
mean anomaly at epoch: | 357.2827° |
orbit number at epoch: | 11089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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