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 23027.32183389 .00009529 00000-0 46067-3 0 9992
2 53807 53.2048 356.9541 0012711 350.2905 9.7844 15.19220576 21021
Epoch (UTC): | 27 January 2023 07:43:26 |
Eccentricity: | 0.0012711 |
inclination: | 53.2048° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 356.9541° |
argument of perigee: | 350.2905° |
revolutions per day: | 15.19220576 |
mean anomaly at epoch: | 9.7844° |
orbit number at epoch: | 2102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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