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 18313U 87068B 22146.16354286 .00000034 00000-0 17070-4 0 9991
2 18313 82.5602 38.3633 0008708 279.2160 80.8015 13.84200599756873
Epoch (UTC): | 26 May 2022 03:55:30 |
Eccentricity: | 0.0008708 |
inclination: | 82.5602° |
perigee height: | 942 km |
apogee height: | 955 km |
right ascension of ascending node: | 38.3633° |
argument of perigee: | 279.2160° |
revolutions per day: | 13.84200599 |
mean anomaly at epoch: | 80.8015° |
orbit number at epoch: | 75687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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