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 11327U 79030B 21104.37179073 -.00000007 00000-0 -22231-4 0 9991
2 11327 82.9505 338.4852 0026708 226.8158 307.5745 13.76961549111198
Epoch (UTC): | 14 April 2021 08:55:22 |
Eccentricity: | 0.0026708 |
inclination: | 82.9505° |
perigee height: | 955 km |
apogee height: | 994 km |
right ascension of ascending node: | 338.4852° |
argument of perigee: | 226.8158° |
revolutions per day: | 13.76961549 |
mean anomaly at epoch: | 307.5745° |
orbit number at epoch: | 11119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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