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 40931U 15052B 24337.09180034 .00002217 00000-0 20975-3 0 9992
2 40931 5.9986 232.5457 0013173 302.5393 57.3463 14.78392648496340
Epoch (UTC): | 02 December 2024 02:12:11 |
Eccentricity: | 0.0013173 |
inclination: | 5.9986° |
perigee height: | 625 km |
apogee height: | 643 km |
right ascension of ascending node: | 232.5457° |
argument of perigee: | 302.5393° |
revolutions per day: | 14.78392648 |
mean anomaly at epoch: | 57.3463° |
orbit number at epoch: | 49634 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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