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 23340.08190019 .00016372 00000-0 52770-3 0 9991
2 40906 97.4914 348.4195 0008078 278.3517 81.6809 15.32225204454668
Epoch (UTC): | 06 December 2023 01:57:56 |
Eccentricity: | 0.0008078 |
inclination: | 97.4914° |
perigee height: | 463 km |
apogee height: | 475 km |
right ascension of ascending node: | 348.4195° |
argument of perigee: | 278.3517° |
revolutions per day: | 15.32225204 |
mean anomaly at epoch: | 81.6809° |
orbit number at epoch: | 45466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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