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 32357U 99025CZA 22176.20130969 .00002332 00000-0 14056-2 0 9991
2 32357 98.8941 311.3602 0563227 234.6337 252.8179 13.49094410495973
Epoch (UTC): | 25 June 2022 04:49:53 |
Eccentricity: | 0.0563227 |
inclination: | 98.8941° |
perigee height: | 656 km |
apogee height: | 1495 km |
right ascension of ascending node: | 311.3602° |
argument of perigee: | 234.6337° |
revolutions per day: | 13.49094410 |
mean anomaly at epoch: | 252.8179° |
orbit number at epoch: | 49597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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