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 23079.14485054 .00017335 00000-0 71754-3 0 9996
2 40906 97.4970 86.1261 0014586 111.2170 311.6336 15.23906233414824
Epoch (UTC): | 20 March 2023 03:28:35 |
Eccentricity: | 0.0014586 |
inclination: | 97.4970° |
perigee height: | 484 km |
apogee height: | 504 km |
right ascension of ascending node: | 86.1261° |
argument of perigee: | 111.2170° |
revolutions per day: | 15.23906233 |
mean anomaly at epoch: | 311.6336° |
orbit number at epoch: | 41482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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