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 23028.90070983 .00006560 00000-0 32181-3 0 9996
2 53807 53.2051 349.7501 0012851 355.3566 4.7309 15.19243883 21268
Epoch (UTC): | 28 January 2023 21:37:01 |
Eccentricity: | 0.0012851 |
inclination: | 53.2051° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 349.7501° |
argument of perigee: | 355.3566° |
revolutions per day: | 15.19243883 |
mean anomaly at epoch: | 4.7309° |
orbit number at epoch: | 2126 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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