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 11870U 80056B 24357.84128711 .00000520 00000-0 18023-3 0 9993
2 11870 74.0511 203.3350 0016479 196.2400 163.8228 14.37991219305376
Epoch (UTC): | 22 December 2024 20:11:27 |
Eccentricity: | 0.0016479 |
inclination: | 74.0511° |
perigee height: | 753 km |
apogee height: | 777 km |
right ascension of ascending node: | 203.3350° |
argument of perigee: | 196.2400° |
revolutions per day: | 14.37991219 |
mean anomaly at epoch: | 163.8228° |
orbit number at epoch: | 30537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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