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 19336U 88064A 24358.13698892 .00000069 00000-0 14510-3 0 9995
2 19336 82.5435 353.8714 0018162 118.2981 310.9582 13.17257404750655
Epoch (UTC): | 23 December 2024 03:17:15 |
Eccentricity: | 0.0018162 |
inclination: | 82.5435° |
perigee height: | 1181 km |
apogee height: | 1209 km |
right ascension of ascending node: | 353.8714° |
argument of perigee: | 118.2981° |
revolutions per day: | 13.17257404 |
mean anomaly at epoch: | 310.9582° |
orbit number at epoch: | 75065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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