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 30243U 99025XC 24357.28195694 .00001232 00000-0 69232-3 0 9995
2 30243 98.7098 12.7971 0013043 56.3979 4.3597 14.12292618922605
Epoch (UTC): | 22 December 2024 06:46:01 |
Eccentricity: | 0.0013043 |
inclination: | 98.7098° |
perigee height: | 842 km |
apogee height: | 861 km |
right ascension of ascending node: | 12.7971° |
argument of perigee: | 56.3979° |
revolutions per day: | 14.12292618 |
mean anomaly at epoch: | 4.3597° |
orbit number at epoch: | 92260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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