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 53807U 22111AL 24357.38932601 .00009929 00000-0 33706-3 0 9994
2 53807 53.2354 43.3191 0006938 318.2728 41.7744 15.31130676127016
Epoch (UTC): | 22 December 2024 09:20:37 |
Eccentricity: | 0.0006938 |
inclination: | 53.2354° |
perigee height: | 467 km |
apogee height: | 477 km |
right ascension of ascending node: | 43.3191° |
argument of perigee: | 318.2728° |
revolutions per day: | 15.31130676 |
mean anomaly at epoch: | 41.7744° |
orbit number at epoch: | 12701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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