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 24260.95687195 .00011865 00000-0 43692-3 0 9992
2 53807 53.2356 130.1589 0008399 28.6522 331.4939 15.28257310112257
Epoch (UTC): | 16 September 2024 22:57:53 |
Eccentricity: | 0.0008399 |
inclination: | 53.2356° |
perigee height: | 475 km |
apogee height: | 487 km |
right ascension of ascending node: | 130.1589° |
argument of perigee: | 28.6522° |
revolutions per day: | 15.28257310 |
mean anomaly at epoch: | 331.4939° |
orbit number at epoch: | 11225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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