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 40912U 15049P 23030.33896569 .00026580 00000-0 83496-3 0 9996
2 40912 97.4299 46.4478 0009640 205.5799 280.0218 15.32933004408415
Epoch (UTC): | 30 January 2023 08:08:06 |
Eccentricity: | 0.0009640 |
inclination: | 97.4299° |
perigee height: | 460 km |
apogee height: | 473 km |
right ascension of ascending node: | 46.4478° |
argument of perigee: | 205.5799° |
revolutions per day: | 15.32933004 |
mean anomaly at epoch: | 280.0218° |
orbit number at epoch: | 40841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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