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 14552U 83122B 22145.15058833 .00000401 00000-0 45613-4 0 9998
2 14552 82.5249 188.5034 0016499 338.6761 21.3765 14.83677204 76482
Epoch (UTC): | 25 May 2022 03:36:50 |
Eccentricity: | 0.0016499 |
inclination: | 82.5249° |
perigee height: | 606 km |
apogee height: | 629 km |
right ascension of ascending node: | 188.5034° |
argument of perigee: | 338.6761° |
revolutions per day: | 14.83677204 |
mean anomaly at epoch: | 21.3765° |
orbit number at epoch: | 7648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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