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 40043U 14033AK 23331.46285090 .00003838 00000-0 53263-3 0 9992
2 40043 97.6738 138.4559 0055678 242.7432 116.8101 14.77415009507517
Epoch (UTC): | 27 November 2023 11:06:30 |
Eccentricity: | 0.0055678 |
inclination: | 97.6738° |
perigee height: | 598 km |
apogee height: | 676 km |
right ascension of ascending node: | 138.4559° |
argument of perigee: | 242.7432° |
revolutions per day: | 14.77415009 |
mean anomaly at epoch: | 116.8101° |
orbit number at epoch: | 50751 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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