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 23156.32410616 .00005102 00000-0 24276-3 0 9992
2 53807 53.1987 127.5416 0013723 16.9596 343.1857 15.20785616 40642
Epoch (UTC): | 05 June 2023 07:46:42 |
Eccentricity: | 0.0013723 |
inclination: | 53.1987° |
perigee height: | 494 km |
apogee height: | 513 km |
right ascension of ascending node: | 127.5416° |
argument of perigee: | 16.9596° |
revolutions per day: | 15.20785616 |
mean anomaly at epoch: | 343.1857° |
orbit number at epoch: | 4064 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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