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 24280.14591014 .00099677 00000-0 14864-2 0 9992
2 40906 97.4692 300.6391 0004019 236.5473 123.5397 15.54728241501638
Epoch (UTC): | 06 October 2024 03:30:06 |
Eccentricity: | 0.0004019 |
inclination: | 97.4692° |
perigee height: | 400 km |
apogee height: | 405 km |
right ascension of ascending node: | 300.6391° |
argument of perigee: | 236.5473° |
revolutions per day: | 15.54728241 |
mean anomaly at epoch: | 123.5397° |
orbit number at epoch: | 50163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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