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 55909U 23035B 23335.23437172 .00015191 00000-0 13635-2 0 9993
2 55909 44.0022 27.8244 0009209 348.0881 11.9755 14.95567173 38750
Epoch (UTC): | 01 December 2023 05:37:29 |
Eccentricity: | 0.0009209 |
inclination: | 44.0022° |
perigee height: | 574 km |
apogee height: | 587 km |
right ascension of ascending node: | 27.8244° |
argument of perigee: | 348.0881° |
revolutions per day: | 14.95567173 |
mean anomaly at epoch: | 11.9755° |
orbit number at epoch: | 3875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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