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 43775U 18099T 24358.11325959 .00006919 00000-0 49705-3 0 9993
2 43775 97.4997 47.4573 0006935 31.1708 328.9928 15.04572481330785
Epoch (UTC): | 23 December 2024 02:43:05 |
Eccentricity: | 0.0006935 |
inclination: | 97.4997° |
perigee height: | 548 km |
apogee height: | 557 km |
right ascension of ascending node: | 47.4573° |
argument of perigee: | 31.1708° |
revolutions per day: | 15.04572481 |
mean anomaly at epoch: | 328.9928° |
orbit number at epoch: | 33078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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