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 27422U 02021B 22222.83579716 .00000099 00000-0 55288-4 0 9998
2 27422 98.4513 167.2076 0013449 77.2488 283.0197 14.29435339 57224
Epoch (UTC): | 10 August 2022 20:03:32 |
Eccentricity: | 0.0013449 |
inclination: | 98.4513° |
perigee height: | 784 km |
apogee height: | 803 km |
right ascension of ascending node: | 167.2076° |
argument of perigee: | 77.2488° |
revolutions per day: | 14.29435339 |
mean anomaly at epoch: | 283.0197° |
orbit number at epoch: | 5722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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