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 14051U 83041B 24284.22125267 .00023082 00000-0 21096-2 0 9999
2 14051 25.3344 237.9633 1023680 310.9913 40.6330 13.25310120929793
Epoch (UTC): | 10 October 2024 05:18:36 |
Eccentricity: | 0.1023680 |
inclination: | 25.3344° |
perigee height: | 392 km |
apogee height: | 1936 km |
right ascension of ascending node: | 237.9633° |
argument of perigee: | 310.9913° |
revolutions per day: | 13.25310120 |
mean anomaly at epoch: | 40.6330° |
orbit number at epoch: | 92979 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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