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 25544U 98067A 24260.01287390 -.00166299 00000-0 -30612-2 0 9993
2 25544 51.6354 225.4806 0007131 0.3087 107.0583 15.49092619472635
Epoch (UTC): | 16 September 2024 00:18:32 |
Eccentricity: | 0.0007131 |
inclination: | 51.6354° |
perigee height: | 414 km |
apogee height: | 424 km |
right ascension of ascending node: | 225.4806° |
argument of perigee: | 0.3087° |
revolutions per day: | 15.49092619 |
mean anomaly at epoch: | 107.0583° |
orbit number at epoch: | 47263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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