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 18214U 87062A 23156.39531088 .00005805 00000-0 32459-3 0 9997
2 18214 82.5198 126.2891 0028571 356.6904 3.4133 15.12940325935841
Epoch (UTC): | 05 June 2023 09:29:14 |
Eccentricity: | 0.0028571 |
inclination: | 82.5198° |
perigee height: | 507 km |
apogee height: | 547 km |
right ascension of ascending node: | 126.2891° |
argument of perigee: | 356.6904° |
revolutions per day: | 15.12940325 |
mean anomaly at epoch: | 3.4133° |
orbit number at epoch: | 93584 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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