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 23026.33502301 .00007570 00000-0 36947-3 0 9991
2 53807 53.2043 1.4566 0012629 346.9525 13.1143 15.19195857 20879
Epoch (UTC): | 26 January 2023 08:02:25 |
Eccentricity: | 0.0012629 |
inclination: | 53.2043° |
perigee height: | 499 km |
apogee height: | 517 km |
right ascension of ascending node: | 1.4566° |
argument of perigee: | 346.9525° |
revolutions per day: | 15.19195857 |
mean anomaly at epoch: | 13.1143° |
orbit number at epoch: | 2087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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