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 32052U 07038A 23082.88164385 .00000086 00000-0 73810-4 0 9995
2 32052 82.9855 356.4313 0037233 295.1922 64.5375 13.74990642779305
Epoch (UTC): | 23 March 2023 21:09:34 |
Eccentricity: | 0.0037233 |
inclination: | 82.9855° |
perigee height: | 954 km |
apogee height: | 1009 km |
right ascension of ascending node: | 356.4313° |
argument of perigee: | 295.1922° |
revolutions per day: | 13.74990642 |
mean anomaly at epoch: | 64.5375° |
orbit number at epoch: | 77930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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