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 35933U 09051C 23340.56187815 .00001076 00000-0 24396-3 0 9992
2 35933 98.4873 215.9629 0005009 197.2730 162.8298 14.58132866754489
Epoch (UTC): | 06 December 2023 13:29:06 |
Eccentricity: | 0.0005009 |
inclination: | 98.4873° |
perigee height: | 695 km |
apogee height: | 703 km |
right ascension of ascending node: | 215.9629° |
argument of perigee: | 197.2730° |
revolutions per day: | 14.58132866 |
mean anomaly at epoch: | 162.8298° |
orbit number at epoch: | 75448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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