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 33591U 09005A 24315.79793884 .00000677 00000-0 38595-3 0 9998
2 33591 99.0291 13.0284 0013015 236.4744 123.5185 14.13195354812339
Epoch (UTC): | 10 November 2024 19:09:01 |
Eccentricity: | 0.0013015 |
inclination: | 99.0291° |
perigee height: | 839 km |
apogee height: | 858 km |
right ascension of ascending node: | 13.0284° |
argument of perigee: | 236.4744° |
revolutions per day: | 14.13195354 |
mean anomaly at epoch: | 123.5185° |
orbit number at epoch: | 81233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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