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 25140.18628703 .00004963 00000-0 16591-3 0 9994
2 53807 53.2321 71.3370 0008997 51.9114 308.2699 15.32794983149828
Epoch (UTC): | 20 May 2025 04:28:15 |
Eccentricity: | 0.0008997 |
inclination: | 53.2321° |
perigee height: | 461 km |
apogee height: | 473 km |
right ascension of ascending node: | 71.3370° |
argument of perigee: | 51.9114° |
revolutions per day: | 15.32794983 |
mean anomaly at epoch: | 308.2699° |
orbit number at epoch: | 14982 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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