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 22826U 93061D 24357.74575304 .00000300 00000-0 13111-3 0 9998
2 22826 98.7586 52.1276 0008167 227.4582 132.5912 14.31087516629860
Epoch (UTC): | 22 December 2024 17:53:53 |
Eccentricity: | 0.0008167 |
inclination: | 98.7586° |
perigee height: | 782 km |
apogee height: | 794 km |
right ascension of ascending node: | 52.1276° |
argument of perigee: | 227.4582° |
revolutions per day: | 14.31087516 |
mean anomaly at epoch: | 132.5912° |
orbit number at epoch: | 62986 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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