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 48178U 02032T 24357.41102710 .00014348 00000-0 43230-2 0 9996
2 48178 98.8524 335.8836 0012449 70.2898 289.9632 14.42586833195532
Epoch (UTC): | 22 December 2024 09:51:52 |
Eccentricity: | 0.0012449 |
inclination: | 98.8524° |
perigee height: | 741 km |
apogee height: | 759 km |
right ascension of ascending node: | 335.8836° |
argument of perigee: | 70.2898° |
revolutions per day: | 14.42586833 |
mean anomaly at epoch: | 289.9632° |
orbit number at epoch: | 19553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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