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 23157.36588041 .00014385 00000-0 53033-3 0 9995
2 40911 97.4889 165.4165 0010771 183.4973 176.6193 15.27858561426712
Epoch (UTC): | 06 June 2023 08:46:52 |
Eccentricity: | 0.0010771 |
inclination: | 97.4889° |
perigee height: | 475 km |
apogee height: | 489 km |
right ascension of ascending node: | 165.4165° |
argument of perigee: | 183.4973° |
revolutions per day: | 15.27858561 |
mean anomaly at epoch: | 176.6193° |
orbit number at epoch: | 42671 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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