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 23332.60174661 .00002203 00000-0 48886-3 0 9996
2 35933 98.4878 207.8387 0004580 226.2513 133.8306 14.58101229753240
Epoch (UTC): | 28 November 2023 14:26:30 |
Eccentricity: | 0.0004580 |
inclination: | 98.4878° |
perigee height: | 696 km |
apogee height: | 702 km |
right ascension of ascending node: | 207.8387° |
argument of perigee: | 226.2513° |
revolutions per day: | 14.58101229 |
mean anomaly at epoch: | 133.8306° |
orbit number at epoch: | 75324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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