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 23333.42693032 .00004668 00000-0 64580-3 0 9995
2 40043 97.6739 140.3264 0055731 236.2566 123.3328 14.77435697507800
Epoch (UTC): | 29 November 2023 10:14:46 |
Eccentricity: | 0.0055731 |
inclination: | 97.6739° |
perigee height: | 598 km |
apogee height: | 676 km |
right ascension of ascending node: | 140.3264° |
argument of perigee: | 236.2566° |
revolutions per day: | 14.77435697 |
mean anomaly at epoch: | 123.3328° |
orbit number at epoch: | 50780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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