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 37418U 99025EGL 23330.60981767 .00001995 00000-0 52593-2 0 9993
2 37418 98.6216 102.2397 1069120 353.1138 5.6173 11.92414068405696
Epoch (UTC): | 26 November 2023 14:38:08 |
Eccentricity: | 0.1069120 |
inclination: | 98.6216° |
perigee height: | 850 km |
apogee height: | 2580 km |
right ascension of ascending node: | 102.2397° |
argument of perigee: | 353.1138° |
revolutions per day: | 11.92414068 |
mean anomaly at epoch: | 5.6173° |
orbit number at epoch: | 40569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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