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 24287.43650211 .00013480 00000-0 48165-3 0 9998
2 53807 53.2367 7.6713 0008977 91.7852 268.4177 15.29124661116301
Epoch (UTC): | 13 October 2024 10:28:33 |
Eccentricity: | 0.0008977 |
inclination: | 53.2367° |
perigee height: | 472 km |
apogee height: | 484 km |
right ascension of ascending node: | 7.6713° |
argument of perigee: | 91.7852° |
revolutions per day: | 15.29124661 |
mean anomaly at epoch: | 268.4177° |
orbit number at epoch: | 11630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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