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 36258U 99025DWK 24356.77645335 .00003472 00000-0 43959-3 0 9998
2 36258 99.0894 337.3157 0181643 151.2031 209.9348 14.71620697855804
Epoch (UTC): | 21 December 2024 18:38:05 |
Eccentricity: | 0.0181643 |
inclination: | 99.0894° |
perigee height: | 528 km |
apogee height: | 783 km |
right ascension of ascending node: | 337.3157° |
argument of perigee: | 151.2031° |
revolutions per day: | 14.71620697 |
mean anomaly at epoch: | 209.9348° |
orbit number at epoch: | 85580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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