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 23333.63108474 .00002406 00000-0 53283-3 0 9991
2 35933 98.4877 208.8892 0004667 222.2911 137.7928 14.58106819753473
Epoch (UTC): | 29 November 2023 15:08:45 |
Eccentricity: | 0.0004667 |
inclination: | 98.4877° |
perigee height: | 696 km |
apogee height: | 702 km |
right ascension of ascending node: | 208.8892° |
argument of perigee: | 222.2911° |
revolutions per day: | 14.58106819 |
mean anomaly at epoch: | 137.7928° |
orbit number at epoch: | 75347 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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