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 11681U 80007B 22224.79294792 .00000087 00000-0 74177-4 0 9998
2 11681 82.9295 96.5217 0037163 133.2804 298.9829 13.75491451131164
Epoch (UTC): | 12 August 2022 19:01:50 |
Eccentricity: | 0.0037163 |
inclination: | 82.9295° |
perigee height: | 952 km |
apogee height: | 1007 km |
right ascension of ascending node: | 96.5217° |
argument of perigee: | 133.2804° |
revolutions per day: | 13.75491451 |
mean anomaly at epoch: | 298.9829° |
orbit number at epoch: | 13116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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