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 15427U 84123A 23333.99681417 .00000328 00000-0 18819-3 0 9999
2 15427 99.1061 321.6796 0015741 102.0607 326.2716 14.16463712 11942
Epoch (UTC): | 29 November 2023 23:55:24 |
Eccentricity: | 0.0015741 |
inclination: | 99.1061° |
perigee height: | 826 km |
apogee height: | 848 km |
right ascension of ascending node: | 321.6796° |
argument of perigee: | 102.0607° |
revolutions per day: | 14.16463712 |
mean anomaly at epoch: | 326.2716° |
orbit number at epoch: | 1194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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