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 22224.79573386 .00000106 00000-0 57928-4 0 9994
2 27422 98.4513 169.1093 0013430 71.9967 288.2678 14.29435970 57500
Epoch (UTC): | 12 August 2022 19:05:51 |
Eccentricity: | 0.0013430 |
inclination: | 98.4513° |
perigee height: | 784 km |
apogee height: | 803 km |
right ascension of ascending node: | 169.1093° |
argument of perigee: | 71.9967° |
revolutions per day: | 14.29435970 |
mean anomaly at epoch: | 288.2678° |
orbit number at epoch: | 5750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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