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 23336.00051347 .00005856 00000-0 80765-3 0 9992
2 40043 97.6745 142.7773 0055793 227.7303 131.9170 14.77464152508483
Epoch (UTC): | 02 December 2023 00:00:44 |
Eccentricity: | 0.0055793 |
inclination: | 97.6745° |
perigee height: | 598 km |
apogee height: | 676 km |
right ascension of ascending node: | 142.7773° |
argument of perigee: | 227.7303° |
revolutions per day: | 14.77464152 |
mean anomaly at epoch: | 131.9170° |
orbit number at epoch: | 50848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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