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 40931U 15052B 23337.40314487 .00001702 00000-0 14444-3 0 9999
2 40931 6.0012 318.3939 0012912 174.6405 185.3862 14.77506852442307
Epoch (UTC): | 03 December 2023 09:40:31 |
Eccentricity: | 0.0012912 |
inclination: | 6.0012° |
perigee height: | 628 km |
apogee height: | 646 km |
right ascension of ascending node: | 318.3939° |
argument of perigee: | 174.6405° |
revolutions per day: | 14.77506852 |
mean anomaly at epoch: | 185.3862° |
orbit number at epoch: | 44230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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