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 23033.24253486 .00004586 00000-0 22935-3 0 9992
2 53807 53.2066 329.9381 0013154 8.3554 351.7659 15.19283912 21922
Epoch (UTC): | 02 February 2023 05:49:15 |
Eccentricity: | 0.0013154 |
inclination: | 53.2066° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 329.9381° |
argument of perigee: | 8.3554° |
revolutions per day: | 15.19283912 |
mean anomaly at epoch: | 351.7659° |
orbit number at epoch: | 2192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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