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 43678U 18084H 22141.76021000 .00001309 00000-0 13443-3 0 9996
2 43678 97.9661 274.7201 0010418 21.3734 338.7913 14.92124742193873
Epoch (UTC): | 21 May 2022 18:14:42 |
Eccentricity: | 0.0010418 |
inclination: | 97.9661° |
perigee height: | 584 km |
apogee height: | 598 km |
right ascension of ascending node: | 274.7201° |
argument of perigee: | 21.3734° |
revolutions per day: | 14.92124742 |
mean anomaly at epoch: | 338.7913° |
orbit number at epoch: | 19387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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