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 11574U 79089B 23152.38500034 .00000336 00000-0 11224-3 0 9992
2 11574 74.0675 163.0816 0016941 236.4051 123.5488 14.41155036290211
Epoch (UTC): | 01 June 2023 09:14:24 |
Eccentricity: | 0.0016941 |
inclination: | 74.0675° |
perigee height: | 742 km |
apogee height: | 767 km |
right ascension of ascending node: | 163.0816° |
argument of perigee: | 236.4051° |
revolutions per day: | 14.41155036 |
mean anomaly at epoch: | 123.5488° |
orbit number at epoch: | 29021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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