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 34729U 93036YX 24357.08507939 .00020819 00000-0 34013-2 0 9991
2 34729 74.0229 336.3043 0019925 204.1853 276.1105 14.70691755832507
Epoch (UTC): | 22 December 2024 02:02:30 |
Eccentricity: | 0.0019925 |
inclination: | 74.0229° |
perigee height: | 645 km |
apogee height: | 673 km |
right ascension of ascending node: | 336.3043° |
argument of perigee: | 204.1853° |
revolutions per day: | 14.70691755 |
mean anomaly at epoch: | 276.1105° |
orbit number at epoch: | 83250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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