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 22145.55276704 .00000495 00000-0 56420-4 0 9996
2 14373 82.5404 358.9234 0021077 38.2146 322.0558 14.83961550 67200
Epoch (UTC): | 25 May 2022 13:15:59 |
Eccentricity: | 0.0021077 |
inclination: | 82.5404° |
perigee height: | 602 km |
apogee height: | 631 km |
right ascension of ascending node: | 358.9234° |
argument of perigee: | 38.2146° |
revolutions per day: | 14.83961550 |
mean anomaly at epoch: | 322.0558° |
orbit number at epoch: | 6720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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