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 54576U 22151MC 23339.04232544 .00010831 00000-0 32320-2 0 9997
2 54576 98.6806 351.4237 0104079 245.6082 113.4216 14.40062079 54964
Epoch (UTC): | 05 December 2023 01:00:56 |
Eccentricity: | 0.0104079 |
inclination: | 98.6806° |
perigee height: | 684 km |
apogee height: | 832 km |
right ascension of ascending node: | 351.4237° |
argument of perigee: | 245.6082° |
revolutions per day: | 14.40062079 |
mean anomaly at epoch: | 113.4216° |
orbit number at epoch: | 5496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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