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 24261.01024118 .00069037 00000-0 11492-2 0 9994
2 40906 97.4726 280.7146 0004494 349.3942 10.7215 15.51788883498662
Epoch (UTC): | 17 September 2024 00:14:44 |
Eccentricity: | 0.0004494 |
inclination: | 97.4726° |
perigee height: | 408 km |
apogee height: | 414 km |
right ascension of ascending node: | 280.7146° |
argument of perigee: | 349.3942° |
revolutions per day: | 15.51788883 |
mean anomaly at epoch: | 10.7215° |
orbit number at epoch: | 49866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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