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 40336U 14079A 24259.94145967 .00000738 00000-0 27139-3 0 9997
2 40336 98.3923 325.8706 0001944 84.2404 275.9003 14.35502839512243
Epoch (UTC): | 15 September 2024 22:35:42 |
Eccentricity: | 0.0001944 |
inclination: | 98.3923° |
perigee height: | 772 km |
apogee height: | 775 km |
right ascension of ascending node: | 325.8706° |
argument of perigee: | 84.2404° |
revolutions per day: | 14.35502839 |
mean anomaly at epoch: | 275.9003° |
orbit number at epoch: | 51224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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