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 23160.26720553 .00005463 00000-0 25851-3 0 9994
2 53807 53.2014 109.5045 0014144 28.6792 331.4980 15.20830624 41242
Epoch (UTC): | 09 June 2023 06:24:46 |
Eccentricity: | 0.0014144 |
inclination: | 53.2014° |
perigee height: | 493 km |
apogee height: | 513 km |
right ascension of ascending node: | 109.5045° |
argument of perigee: | 28.6792° |
revolutions per day: | 15.20830624 |
mean anomaly at epoch: | 331.4980° |
orbit number at epoch: | 4124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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