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 18422U 87088B 23156.45387454 .00000521 00000-0 60057-4 0 9995
2 18422 82.5106 294.3047 0020882 99.2172 261.1406 14.83584629903732
Epoch (UTC): | 05 June 2023 10:53:34 |
Eccentricity: | 0.0020882 |
inclination: | 82.5106° |
perigee height: | 603 km |
apogee height: | 632 km |
right ascension of ascending node: | 294.3047° |
argument of perigee: | 99.2172° |
revolutions per day: | 14.83584629 |
mean anomaly at epoch: | 261.1406° |
orbit number at epoch: | 90373 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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