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 24357.53290572 .00155822 00000-0 11131-2 0 9994
2 40906 97.4534 22.3380 0003462 8.7267 351.4057 15.73295859513723
Epoch (UTC): | 22 December 2024 12:47:23 |
Eccentricity: | 0.0003462 |
inclination: | 97.4534° |
perigee height: | 347 km |
apogee height: | 352 km |
right ascension of ascending node: | 22.3380° |
argument of perigee: | 8.7267° |
revolutions per day: | 15.73295859 |
mean anomaly at epoch: | 351.4057° |
orbit number at epoch: | 51372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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