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 43803U 18099AX 24357.69066837 .00016521 00000-0 89854-3 0 9993
2 43803 97.4952 52.7658 0008751 22.7569 337.4049 15.14511247331155
Epoch (UTC): | 22 December 2024 16:34:33 |
Eccentricity: | 0.0008751 |
inclination: | 97.4952° |
perigee height: | 516 km |
apogee height: | 528 km |
right ascension of ascending node: | 52.7658° |
argument of perigee: | 22.7569° |
revolutions per day: | 15.14511247 |
mean anomaly at epoch: | 337.4049° |
orbit number at epoch: | 33115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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