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 25893U 99045B 22222.63205934 -.00000003 00000-0 -18725-4 0 9998
2 25893 82.9233 64.7012 0027513 235.1536 157.5041 13.76587931153360
Epoch (UTC): | 10 August 2022 15:10:09 |
Eccentricity: | 0.0027513 |
inclination: | 82.9233° |
perigee height: | 956 km |
apogee height: | 996 km |
right ascension of ascending node: | 64.7012° |
argument of perigee: | 235.1536° |
revolutions per day: | 13.76587931 |
mean anomaly at epoch: | 157.5041° |
orbit number at epoch: | 15336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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