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 54525U 22151KD 24357.92548923 .00000561 00000-0 36564-3 0 9994
2 54525 98.8198 350.0383 0070232 92.9951 267.9256 14.05179984108124
Epoch (UTC): | 22 December 2024 22:12:42 |
Eccentricity: | 0.0070232 |
inclination: | 98.8198° |
perigee height: | 825 km |
apogee height: | 927 km |
right ascension of ascending node: | 350.0383° |
argument of perigee: | 92.9951° |
revolutions per day: | 14.05179984 |
mean anomaly at epoch: | 267.9256° |
orbit number at epoch: | 10812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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