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 46U 60007B 22146.84817754 .00000322 00000-0 85261-4 0 9995
2 46 66.6900 292.0539 0214117 321.3940 37.2019 14.49687559241767
Epoch (UTC): | 26 May 2022 20:21:22 |
Eccentricity: | 0.0214117 |
inclination: | 66.6900° |
perigee height: | 574 km |
apogee height: | 879 km |
right ascension of ascending node: | 292.0539° |
argument of perigee: | 321.3940° |
revolutions per day: | 14.49687559 |
mean anomaly at epoch: | 37.2019° |
orbit number at epoch: | 24176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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