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 43137U 18004AC 23340.21822731 .00143325 00000-0 10641-2 0 9991
2 43137 97.3073 63.5159 0003362 232.6946 127.4012 15.72421379329051
Epoch (UTC): | 06 December 2023 05:14:14 |
Eccentricity: | 0.0003362 |
inclination: | 97.3073° |
perigee height: | 350 km |
apogee height: | 354 km |
right ascension of ascending node: | 63.5159° |
argument of perigee: | 232.6946° |
revolutions per day: | 15.72421379 |
mean anomaly at epoch: | 127.4012° |
orbit number at epoch: | 32905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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