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 22081U 92053B 23161.18565200 .00000241 00000-0 95153-4 0 9996
2 22081 74.0454 46.2236 0036408 201.8253 158.1350 14.33825038611798
Epoch (UTC): | 10 June 2023 04:27:20 |
Eccentricity: | 0.0036408 |
inclination: | 74.0454° |
perigee height: | 753 km |
apogee height: | 805 km |
right ascension of ascending node: | 46.2236° |
argument of perigee: | 201.8253° |
revolutions per day: | 14.33825038 |
mean anomaly at epoch: | 158.1350° |
orbit number at epoch: | 61179 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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