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 24318.18591510 .00000915 00000-0 31107-3 0 9994
2 11870 74.0520 276.2883 0017528 275.3222 84.5932 14.37935499323530
Epoch (UTC): | 13 November 2024 04:27:43 |
Eccentricity: | 0.0017528 |
inclination: | 74.0520° |
perigee height: | 753 km |
apogee height: | 778 km |
right ascension of ascending node: | 276.2883° |
argument of perigee: | 275.3222° |
revolutions per day: | 14.37935499 |
mean anomaly at epoch: | 84.5932° |
orbit number at epoch: | 32353 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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