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 40910U 15049M 23089.61780986 .00036056 00000-0 11307-2 0 9994
2 40910 97.4686 101.7261 0012381 55.5035 87.3126 15.32893466416838
Epoch (UTC): | 30 March 2023 14:49:38 |
Eccentricity: | 0.0012381 |
inclination: | 97.4686° |
perigee height: | 459 km |
apogee height: | 475 km |
right ascension of ascending node: | 101.7261° |
argument of perigee: | 55.5035° |
revolutions per day: | 15.32893466 |
mean anomaly at epoch: | 87.3126° |
orbit number at epoch: | 41683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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