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 53U 60009E 22146.91808123 -.00000147 00000-0 -60704-3 0 9994
2 53 47.2752 234.1588 0096960 14.5618 345.7932 12.17270615754868
Epoch (UTC): | 26 May 2022 22:02:02 |
Eccentricity: | 0.0096960 |
inclination: | 47.2752° |
perigee height: | 1527 km |
apogee height: | 1682 km |
right ascension of ascending node: | 234.1588° |
argument of perigee: | 14.5618° |
revolutions per day: | 12.17270615 |
mean anomaly at epoch: | 345.7932° |
orbit number at epoch: | 75486 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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