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 23342.10636603 .00012558 00000-0 40485-3 0 9992
2 40906 97.4910 350.4674 0008044 269.3309 90.7011 15.32282105454974
Epoch (UTC): | 08 December 2023 02:33:10 |
Eccentricity: | 0.0008044 |
inclination: | 97.4910° |
perigee height: | 463 km |
apogee height: | 474 km |
right ascension of ascending node: | 350.4674° |
argument of perigee: | 269.3309° |
revolutions per day: | 15.32282105 |
mean anomaly at epoch: | 90.7011° |
orbit number at epoch: | 45497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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