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 54513U 22151JR 24357.99753296 .00001976 00000-0 56115-3 0 9994
2 54513 98.4941 4.3742 0152434 162.6768 197.9703 14.39939883110724
Epoch (UTC): | 22 December 2024 23:56:26 |
Eccentricity: | 0.0152434 |
inclination: | 98.4941° |
perigee height: | 650 km |
apogee height: | 867 km |
right ascension of ascending node: | 4.3742° |
argument of perigee: | 162.6768° |
revolutions per day: | 14.39939883 |
mean anomaly at epoch: | 197.9703° |
orbit number at epoch: | 11072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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