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 23081.84782703 .00015568 00000-0 64338-3 0 9993
2 40906 97.4972 88.8284 0014775 103.6754 18.6966 15.23982108415237
Epoch (UTC): | 22 March 2023 20:20:52 |
Eccentricity: | 0.0014775 |
inclination: | 97.4972° |
perigee height: | 483 km |
apogee height: | 504 km |
right ascension of ascending node: | 88.8284° |
argument of perigee: | 103.6754° |
revolutions per day: | 15.23982108 |
mean anomaly at epoch: | 18.6966° |
orbit number at epoch: | 41523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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