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 14781U 84021B 24276.81732784 .00008111 00000-0 89842-3 0 9992
2 14781 97.7184 242.9799 0009962 83.1694 277.0655 14.87533815185481
Epoch (UTC): | 02 October 2024 19:36:57 |
Eccentricity: | 0.0009962 |
inclination: | 97.7184° |
perigee height: | 598 km |
apogee height: | 612 km |
right ascension of ascending node: | 242.9799° |
argument of perigee: | 83.1694° |
revolutions per day: | 14.87533815 |
mean anomaly at epoch: | 277.0655° |
orbit number at epoch: | 18548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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