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 22208U 92073B 22228.77777439 -.00000034 00000-0 -51435-4 0 9993
2 22208 82.9152 60.1116 0034405 174.0852 196.2997 13.75191732495034
Epoch (UTC): | 16 August 2022 18:39:59 |
Eccentricity: | 0.0034405 |
inclination: | 82.9152° |
perigee height: | 955 km |
apogee height: | 1006 km |
right ascension of ascending node: | 60.1116° |
argument of perigee: | 174.0852° |
revolutions per day: | 13.75191732 |
mean anomaly at epoch: | 196.2997° |
orbit number at epoch: | 49503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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