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 24308.72497798 .00027431 00000-0 29896-1 0 9997
2 59588 97.4912 344.8878 0041189 182.1593 177.9388 13.72146635 26495
Epoch (UTC): | 03 November 2024 17:23:58 |
Eccentricity: | 0.0041189 |
inclination: | 97.4912° |
perigee height: | 961 km |
apogee height: | 1022 km |
right ascension of ascending node: | 344.8878° |
argument of perigee: | 182.1593° |
revolutions per day: | 13.72146635 |
mean anomaly at epoch: | 177.9388° |
orbit number at epoch: | 2649 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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