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 27760U 94077M 24357.65921148 .00007261 00000-0 14262-2 0 9999
2 27760 70.9950 231.5408 0045060 68.7566 324.2422 14.62322635310692
Epoch (UTC): | 22 December 2024 15:49:15 |
Eccentricity: | 0.0045060 |
inclination: | 70.9950° |
perigee height: | 654 km |
apogee height: | 717 km |
right ascension of ascending node: | 231.5408° |
argument of perigee: | 68.7566° |
revolutions per day: | 14.62322635 |
mean anomaly at epoch: | 324.2422° |
orbit number at epoch: | 31069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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