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 23086.17015931 .00017615 00000-0 72360-3 0 9995
2 40906 97.4969 93.1517 0014525 91.4306 331.0485 15.24160781415897
Epoch (UTC): | 27 March 2023 04:05:01 |
Eccentricity: | 0.0014525 |
inclination: | 97.4969° |
perigee height: | 483 km |
apogee height: | 503 km |
right ascension of ascending node: | 93.1517° |
argument of perigee: | 91.4306° |
revolutions per day: | 15.24160781 |
mean anomaly at epoch: | 331.0485° |
orbit number at epoch: | 41589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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