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 37372U 11009A 23331.58380569 -.00000063 00000-0 00000-0 0 9999
2 37372 65.8485 345.8066 0009214 326.4284 163.0376 2.12910205 99227
Epoch (UTC): | 27 November 2023 14:00:40 |
Eccentricity: | 0.0009214 |
inclination: | 65.8485° |
perigee height: | 19121 km |
apogee height: | 19168 km |
right ascension of ascending node: | 345.8066° |
argument of perigee: | 326.4284° |
revolutions per day: | 2.12910205 |
mean anomaly at epoch: | 163.0376° |
orbit number at epoch: | 9922 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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