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 23332.57085253 .00023405 00000-0 76078-3 0 9991
2 40906 97.4905 340.8246 0008570 311.0593 48.9907 15.31874612453517
Epoch (UTC): | 28 November 2023 13:42:01 |
Eccentricity: | 0.0008570 |
inclination: | 97.4905° |
perigee height: | 464 km |
apogee height: | 476 km |
right ascension of ascending node: | 340.8246° |
argument of perigee: | 311.0593° |
revolutions per day: | 15.31874612 |
mean anomaly at epoch: | 48.9907° |
orbit number at epoch: | 45351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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