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 4749U 70025CX 24358.09843824 .00002282 00000-0 20780-2 0 9991
2 4749 99.0287 202.6308 0016257 17.8798 342.2926 13.84293656728881
Epoch (UTC): | 23 December 2024 02:21:45 |
Eccentricity: | 0.0016257 |
inclination: | 99.0287° |
perigee height: | 937 km |
apogee height: | 960 km |
right ascension of ascending node: | 202.6308° |
argument of perigee: | 17.8798° |
revolutions per day: | 13.84293656 |
mean anomaly at epoch: | 342.2926° |
orbit number at epoch: | 72888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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