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 23340.40260179 .00002909 00000-0 40450-3 0 9999
2 40043 97.6741 146.9691 0055956 213.2650 146.5039 14.77496339508837
Epoch (UTC): | 06 December 2023 09:39:44 |
Eccentricity: | 0.0055956 |
inclination: | 97.6741° |
perigee height: | 598 km |
apogee height: | 676 km |
right ascension of ascending node: | 146.9691° |
argument of perigee: | 213.2650° |
revolutions per day: | 14.77496339 |
mean anomaly at epoch: | 146.5039° |
orbit number at epoch: | 50883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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