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 22144.74603046 .00000034 00000-0 18186-4 0 9990
2 23180 82.9489 29.6583 0028205 208.0367 210.4707 13.78044905400749
Epoch (UTC): | 24 May 2022 17:54:17 |
Eccentricity: | 0.0028205 |
inclination: | 82.9489° |
perigee height: | 950 km |
apogee height: | 991 km |
right ascension of ascending node: | 29.6583° |
argument of perigee: | 208.0367° |
revolutions per day: | 13.78044905 |
mean anomaly at epoch: | 210.4707° |
orbit number at epoch: | 40074 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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