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 40911U 15049N 24317.88001117 .00856973 35793-3 15754-2 0 9999
2 40911 97.4433 345.7291 0002945 143.6548 216.4931 16.01336922507808
Epoch (UTC): | 12 November 2024 21:07:12 |
Eccentricity: | 0.0002945 |
inclination: | 97.4433° |
perigee height: | 269 km |
apogee height: | 272 km |
right ascension of ascending node: | 345.7291° |
argument of perigee: | 143.6548° |
revolutions per day: | 16.01336922 |
mean anomaly at epoch: | 216.4931° |
orbit number at epoch: | 50780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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