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 12U 59001B 22147.02042079 .00000412 00000-0 22481-3 0 9995
2 12 32.9072 31.3980 1665316 201.9146 150.1187 11.44668538603742
Epoch (UTC): | 27 May 2022 00:29:24 |
Eccentricity: | 0.1665316 |
inclination: | 32.9072° |
perigee height: | 553 km |
apogee height: | 3323 km |
right ascension of ascending node: | 31.3980° |
argument of perigee: | 201.9146° |
revolutions per day: | 11.44668538 |
mean anomaly at epoch: | 150.1187° |
orbit number at epoch: | 60374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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