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 11672U 80005B 22144.79175657 .00000527 00000-0 54300-4 0 9990
2 11672 82.5151 177.6720 0018229 92.0885 268.2421 14.88201751270343
Epoch (UTC): | 24 May 2022 19:00:07 |
Eccentricity: | 0.0018229 |
inclination: | 82.5151° |
perigee height: | 591 km |
apogee height: | 616 km |
right ascension of ascending node: | 177.6720° |
argument of perigee: | 92.0885° |
revolutions per day: | 14.88201751 |
mean anomaly at epoch: | 268.2421° |
orbit number at epoch: | 27034 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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