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 24282.84860434 .00105807 00000-0 15411-2 0 9998
2 40906 97.4695 303.4600 0004343 224.1609 135.9298 15.55349783502054
Epoch (UTC): | 08 October 2024 20:21:59 |
Eccentricity: | 0.0004343 |
inclination: | 97.4695° |
perigee height: | 398 km |
apogee height: | 404 km |
right ascension of ascending node: | 303.4600° |
argument of perigee: | 224.1609° |
revolutions per day: | 15.55349783 |
mean anomaly at epoch: | 135.9298° |
orbit number at epoch: | 50205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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