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 24277.69652772 .00019542 00000-0 70057-3 0 9999
2 53807 53.2365 52.7446 0008991 69.1373 291.0590 15.28723037114812
Epoch (UTC): | 03 October 2024 16:42:59 |
Eccentricity: | 0.0008991 |
inclination: | 53.2365° |
perigee height: | 473 km |
apogee height: | 486 km |
right ascension of ascending node: | 52.7446° |
argument of perigee: | 69.1373° |
revolutions per day: | 15.28723037 |
mean anomaly at epoch: | 291.0590° |
orbit number at epoch: | 11481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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