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 10930U 78056A 24358.36271111 -.00000000 00000-0 11347-3 0 9993
2 10930 74.0264 112.7910 0047412 118.6299 297.9732 12.37808758103443
Epoch (UTC): | 23 December 2024 08:42:18 |
Eccentricity: | 0.0047412 |
inclination: | 74.0264° |
perigee height: | 1478 km |
apogee height: | 1553 km |
right ascension of ascending node: | 112.7910° |
argument of perigee: | 118.6299° |
revolutions per day: | 12.37808758 |
mean anomaly at epoch: | 297.9732° |
orbit number at epoch: | 10344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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