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 18986U 88023B 22147.47221406 -.00000015 00000-0 -29769-4 0 9990
2 18986 82.9522 140.4713 0041417 187.6881 172.3648 13.78672146719371
Epoch (UTC): | 27 May 2022 11:19:59 |
Eccentricity: | 0.0041417 |
inclination: | 82.9522° |
perigee height: | 938 km |
apogee height: | 999 km |
right ascension of ascending node: | 140.4713° |
argument of perigee: | 187.6881° |
revolutions per day: | 13.78672146 |
mean anomaly at epoch: | 172.3648° |
orbit number at epoch: | 71937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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