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 40907U 15049J 23334.08203081 .00032575 00000-0 95073-3 0 9995
2 40907 97.4874 343.4675 0006943 295.0622 64.9900 15.35245863453878
Epoch (UTC): | 30 November 2023 01:58:07 |
Eccentricity: | 0.0006943 |
inclination: | 97.4874° |
perigee height: | 455 km |
apogee height: | 465 km |
right ascension of ascending node: | 343.4675° |
argument of perigee: | 295.0622° |
revolutions per day: | 15.35245863 |
mean anomaly at epoch: | 64.9900° |
orbit number at epoch: | 45387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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