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 22825U 93061C 23088.10909277 .00000280 00000-0 12569-3 0 9990
2 22825 98.8520 129.6698 0007496 305.9131 54.1354 14.30273317538843
Epoch (UTC): | 29 March 2023 02:37:05 |
Eccentricity: | 0.0007496 |
inclination: | 98.8520° |
perigee height: | 785 km |
apogee height: | 796 km |
right ascension of ascending node: | 129.6698° |
argument of perigee: | 305.9131° |
revolutions per day: | 14.30273317 |
mean anomaly at epoch: | 54.1354° |
orbit number at epoch: | 53884 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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