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 59588U 24077B 24307.84993581 .00054635 00000-0 59367-1 0 9992
2 59588 97.4874 344.2029 0041839 182.4640 177.6314 13.72080722 26379
Epoch (UTC): | 02 November 2024 20:23:54 |
Eccentricity: | 0.0041839 |
inclination: | 97.4874° |
perigee height: | 961 km |
apogee height: | 1023 km |
right ascension of ascending node: | 344.2029° |
argument of perigee: | 182.4640° |
revolutions per day: | 13.72080722 |
mean anomaly at epoch: | 177.6314° |
orbit number at epoch: | 2637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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