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 24277.10812225 .00025273 00000-0 90207-3 0 9993
2 53807 53.2366 55.4666 0008983 67.8372 292.3582 15.28707131114724
Epoch (UTC): | 03 October 2024 02:35:41 |
Eccentricity: | 0.0008983 |
inclination: | 53.2366° |
perigee height: | 473 km |
apogee height: | 486 km |
right ascension of ascending node: | 55.4666° |
argument of perigee: | 67.8372° |
revolutions per day: | 15.28707131 |
mean anomaly at epoch: | 292.3582° |
orbit number at epoch: | 11472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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