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 40911U 15049N 23332.60799286 .00028865 00000-0 85499-3 0 9991
2 40911 97.4850 342.2906 0007126 303.3196 56.7364 15.34804470453523
Epoch (UTC): | 28 November 2023 14:35:30 |
Eccentricity: | 0.0007126 |
inclination: | 97.4850° |
perigee height: | 456 km |
apogee height: | 466 km |
right ascension of ascending node: | 342.2906° |
argument of perigee: | 303.3196° |
revolutions per day: | 15.34804470 |
mean anomaly at epoch: | 56.7364° |
orbit number at epoch: | 45352 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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