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 45606U 20029A 22224.31724494 0.00000000 00000-0 00000-0 0 03
2 45606 45.0145 275.8418 0010612 284.8979 75.1017 15.78188395 00
Epoch (UTC): | 12 August 2022 07:36:49 |
Eccentricity: | 0.0010612 |
inclination: | 45.0145° |
perigee height: | 328 km |
apogee height: | 343 km |
right ascension of ascending node: | 275.8418° |
argument of perigee: | 284.8979° |
revolutions per day: | 15.78188395 |
mean anomaly at epoch: | 75.1017° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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