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 23081.46721621 .00001620 00000-0 13488-3 0 9999
2 40931 5.9991 345.5614 0012318 144.1101 216.0035 14.77110865404518
Epoch (UTC): | 22 March 2023 11:12:47 |
Eccentricity: | 0.0012318 |
inclination: | 5.9991° |
perigee height: | 630 km |
apogee height: | 647 km |
right ascension of ascending node: | 345.5614° |
argument of perigee: | 144.1101° |
revolutions per day: | 14.77110865 |
mean anomaly at epoch: | 216.0035° |
orbit number at epoch: | 40451 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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