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 14373U 83099B 22147.57562789 .00000385 00000-0 43229-4 0 9992
2 14373 82.5399 357.0318 0020932 31.9375 328.3105 14.83962797 67503
Epoch (UTC): | 27 May 2022 13:48:54 |
Eccentricity: | 0.0020932 |
inclination: | 82.5399° |
perigee height: | 602 km |
apogee height: | 631 km |
right ascension of ascending node: | 357.0318° |
argument of perigee: | 31.9375° |
revolutions per day: | 14.83962797 |
mean anomaly at epoch: | 328.3105° |
orbit number at epoch: | 6750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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