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 23180U 94041B 22141.76944418 .00000075 00000-0 58997-4 0 9999
2 23180 82.9492 31.8733 0028002 216.5746 203.5515 13.78044921400338
Epoch (UTC): | 21 May 2022 18:27:59 |
Eccentricity: | 0.0028002 |
inclination: | 82.9492° |
perigee height: | 950 km |
apogee height: | 991 km |
right ascension of ascending node: | 31.8733° |
argument of perigee: | 216.5746° |
revolutions per day: | 13.78044921 |
mean anomaly at epoch: | 203.5515° |
orbit number at epoch: | 40033 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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