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 12586U 81065B 22147.54803827 .00002776 00000-0 16455-3 0 9991
2 12586 97.6829 141.7858 0019721 124.4851 235.8245 15.12072632224909
Epoch (UTC): | 27 May 2022 13:09:10 |
Eccentricity: | 0.0019721 |
inclination: | 97.6829° |
perigee height: | 516 km |
apogee height: | 543 km |
right ascension of ascending node: | 141.7858° |
argument of perigee: | 124.4851° |
revolutions per day: | 15.12072632 |
mean anomaly at epoch: | 235.8245° |
orbit number at epoch: | 22490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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