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 23149.84415116 .00000519 00000-0 59865-4 0 9999
2 18422 82.5100 300.5062 0020710 119.4705 240.8579 14.83577570902753
Epoch (UTC): | 29 May 2023 20:15:34 |
Eccentricity: | 0.0020710 |
inclination: | 82.5100° |
perigee height: | 603 km |
apogee height: | 632 km |
right ascension of ascending node: | 300.5062° |
argument of perigee: | 119.4705° |
revolutions per day: | 14.83577570 |
mean anomaly at epoch: | 240.8579° |
orbit number at epoch: | 90275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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