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 40906U 15049H 22136.24452637 .00005869 00000-0 28537-3 0 9991
2 40906 97.4931 139.9239 0015810 108.5106 307.4624 15.18689414368039
Epoch (UTC): | 16 May 2022 05:52:07 |
Eccentricity: | 0.0015810 |
inclination: | 97.4931° |
perigee height: | 499 km |
apogee height: | 520 km |
right ascension of ascending node: | 139.9239° |
argument of perigee: | 108.5106° |
revolutions per day: | 15.18689414 |
mean anomaly at epoch: | 307.4624° |
orbit number at epoch: | 36803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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