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 19531U 88089A 24260.89279137 .00000329 00000-0 18947-3 0 9998
2 19531 98.5290 219.4577 0010649 337.1445 22.9254 14.15595423857166
Epoch (UTC): | 16 September 2024 21:25:37 |
Eccentricity: | 0.0010649 |
inclination: | 98.5290° |
perigee height: | 832 km |
apogee height: | 848 km |
right ascension of ascending node: | 219.4577° |
argument of perigee: | 337.1445° |
revolutions per day: | 14.15595423 |
mean anomaly at epoch: | 22.9254° |
orbit number at epoch: | 85716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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