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 23031.26899301 .00004323 00000-0 21718-3 0 9991
2 53807 53.2061 338.9436 0013041 2.4866 357.6193 15.19264254 21627
Epoch (UTC): | 31 January 2023 06:27:20 |
Eccentricity: | 0.0013041 |
inclination: | 53.2061° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 338.9436° |
argument of perigee: | 2.4866° |
revolutions per day: | 15.19264254 |
mean anomaly at epoch: | 357.6193° |
orbit number at epoch: | 2162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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