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 24298U 96051B 24358.17025196 -.00000216 00000-0 -90483-4 0 9998
2 24298 70.7843 29.4218 0014041 60.2155 300.0359 14.12449674459562
Epoch (UTC): | 23 December 2024 04:05:09 |
Eccentricity: | 0.0014041 |
inclination: | 70.7843° |
perigee height: | 841 km |
apogee height: | 861 km |
right ascension of ascending node: | 29.4218° |
argument of perigee: | 60.2155° |
revolutions per day: | 14.12449674 |
mean anomaly at epoch: | 300.0359° |
orbit number at epoch: | 45956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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