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 30760U 99025ATW 24357.94817718 .00000866 00000-0 56023-3 0 9996
2 30760 98.8113 358.5636 0052468 256.3820 103.1501 14.04776706912774
Epoch (UTC): | 22 December 2024 22:45:22 |
Eccentricity: | 0.0052468 |
inclination: | 98.8113° |
perigee height: | 839 km |
apogee height: | 915 km |
right ascension of ascending node: | 358.5636° |
argument of perigee: | 256.3820° |
revolutions per day: | 14.04776706 |
mean anomaly at epoch: | 103.1501° |
orbit number at epoch: | 91277 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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