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 43137U 18004AC 22179.15203095 .00005667 00000-0 20024-3 0 9992
2 43137 97.3689 254.2125 0006424 334.4797 25.6125 15.29580469247975
Epoch (UTC): | 28 June 2022 03:38:55 |
Eccentricity: | 0.0006424 |
inclination: | 97.3689° |
perigee height: | 472 km |
apogee height: | 481 km |
right ascension of ascending node: | 254.2125° |
argument of perigee: | 334.4797° |
revolutions per day: | 15.29580469 |
mean anomaly at epoch: | 25.6125° |
orbit number at epoch: | 24797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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