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 54475U 22151HB 24357.66551604 .00007211 00000-0 13947-2 0 9997
2 54475 98.6630 38.8759 0148591 113.5366 248.1521 14.56812702111644
Epoch (UTC): | 22 December 2024 15:58:20 |
Eccentricity: | 0.0148591 |
inclination: | 98.6630° |
perigee height: | 598 km |
apogee height: | 809 km |
right ascension of ascending node: | 38.8759° |
argument of perigee: | 113.5366° |
revolutions per day: | 14.56812702 |
mean anomaly at epoch: | 248.1521° |
orbit number at epoch: | 11164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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