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 22182.70389945 .00000688 00000-0 64462-4 0 9993
2 43803 97.6188 249.3697 0013950 215.4727 144.5569 14.97133564195209
Epoch (UTC): | 01 July 2022 16:53:36 |
Eccentricity: | 0.0013950 |
inclination: | 97.6188° |
perigee height: | 566 km |
apogee height: | 585 km |
right ascension of ascending node: | 249.3697° |
argument of perigee: | 215.4727° |
revolutions per day: | 14.97133564 |
mean anomaly at epoch: | 144.5569° |
orbit number at epoch: | 19520 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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