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 12792U 81084B 24357.54736851 .00000556 00000-0 19010-3 0 9992
2 12792 74.0300 19.4447 0013878 352.5676 7.5270 14.38606816269288
Epoch (UTC): | 22 December 2024 13:08:12 |
Eccentricity: | 0.0013878 |
inclination: | 74.0300° |
perigee height: | 753 km |
apogee height: | 773 km |
right ascension of ascending node: | 19.4447° |
argument of perigee: | 352.5676° |
revolutions per day: | 14.38606816 |
mean anomaly at epoch: | 7.5270° |
orbit number at epoch: | 26928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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