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 19475U 76126CD 22228.45753904 .00000917 00000-0 52025-3 0 9995
2 19475 65.8294 252.3136 0828637 131.0095 236.5668 13.07803566525712
Epoch (UTC): | 16 August 2022 10:58:51 |
Eccentricity: | 0.0828637 |
inclination: | 65.8294° |
perigee height: | 601 km |
apogee height: | 1862 km |
right ascension of ascending node: | 252.3136° |
argument of perigee: | 131.0095° |
revolutions per day: | 13.07803566 |
mean anomaly at epoch: | 236.5668° |
orbit number at epoch: | 52571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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