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 43803U 18099AX 23089.88538874 .00009905 00000-0 80263-3 0 9993
2 43803 97.5801 154.5053 0014194 23.7223 336.4652 14.99821275235952
Epoch (UTC): | 30 March 2023 21:14:57 |
Eccentricity: | 0.0014194 |
inclination: | 97.5801° |
perigee height: | 557 km |
apogee height: | 577 km |
right ascension of ascending node: | 154.5053° |
argument of perigee: | 23.7223° |
revolutions per day: | 14.99821275 |
mean anomaly at epoch: | 336.4652° |
orbit number at epoch: | 23595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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