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 18095U 87049A 24357.87902519 .00000409 00000-0 15603-3 0 9994
2 18095 74.0393 327.1852 0013582 116.2773 243.9775 14.33865390962304
Epoch (UTC): | 22 December 2024 21:05:47 |
Eccentricity: | 0.0013582 |
inclination: | 74.0393° |
perigee height: | 769 km |
apogee height: | 788 km |
right ascension of ascending node: | 327.1852° |
argument of perigee: | 116.2773° |
revolutions per day: | 14.33865390 |
mean anomaly at epoch: | 243.9775° |
orbit number at epoch: | 96230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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