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 116U 61015A 22146.86715386 .00000030 00000-0 82017-4 0 9995
2 116 66.8099 276.3487 0081337 235.4679 123.8704 13.91829826 90882
Epoch (UTC): | 26 May 2022 20:48:42 |
Eccentricity: | 0.0081337 |
inclination: | 66.8099° |
perigee height: | 863 km |
apogee height: | 981 km |
right ascension of ascending node: | 276.3487° |
argument of perigee: | 235.4679° |
revolutions per day: | 13.91829826 |
mean anomaly at epoch: | 123.8704° |
orbit number at epoch: | 9088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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