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 39265U 13055A 23342.86333327 .00019528 00000-0 44229-3 0 9997
2 39265 80.9595 47.1396 0539099 137.1619 227.2929 14.59714205530386
Epoch (UTC): | 08 December 2023 20:43:11 |
Eccentricity: | 0.0539099 |
inclination: | 80.9595° |
perigee height: | 313 km |
apogee height: | 1075 km |
right ascension of ascending node: | 47.1396° |
argument of perigee: | 137.1619° |
revolutions per day: | 14.59714205 |
mean anomaly at epoch: | 227.2929° |
orbit number at epoch: | 53038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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