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 40792U 93036BVV 24355.33508625 .00007963 00000-0 15999-2 0 9994
2 40792 74.0479 14.3404 0020054 221.1274 150.4146 14.61649855718759
Epoch (UTC): | 20 December 2024 08:02:31 |
Eccentricity: | 0.0020054 |
inclination: | 74.0479° |
perigee height: | 673 km |
apogee height: | 702 km |
right ascension of ascending node: | 14.3404° |
argument of perigee: | 221.1274° |
revolutions per day: | 14.61649855 |
mean anomaly at epoch: | 150.4146° |
orbit number at epoch: | 71875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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