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 43300U 81043X 24353.04399299 .00006712 00000-0 27765-2 0 9993
2 43300 81.2566 245.4897 0028409 179.8165 180.3031 14.26351669477208
Epoch (UTC): | 18 December 2024 01:03:20 |
Eccentricity: | 0.0028409 |
inclination: | 81.2566° |
perigee height: | 783 km |
apogee height: | 824 km |
right ascension of ascending node: | 245.4897° |
argument of perigee: | 179.8165° |
revolutions per day: | 14.26351669 |
mean anomaly at epoch: | 180.3031° |
orbit number at epoch: | 47720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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