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 24310.56929683 .00018384 00000-0 63713-3 0 9995
2 53807 53.2333 260.5313 0008492 148.8911 211.2594 15.29875202119847
Epoch (UTC): | 05 November 2024 13:39:47 |
Eccentricity: | 0.0008492 |
inclination: | 53.2333° |
perigee height: | 470 km |
apogee height: | 482 km |
right ascension of ascending node: | 260.5313° |
argument of perigee: | 148.8911° |
revolutions per day: | 15.29875202 |
mean anomaly at epoch: | 211.2594° |
orbit number at epoch: | 11984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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