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 17974U 87041B 24287.75260282 .00000065 00000-0 55757-4 0 9997
2 17974 71.0103 32.0597 0016203 267.8693 254.0848 14.17506084935533
Epoch (UTC): | 13 October 2024 18:03:44 |
Eccentricity: | 0.0016203 |
inclination: | 71.0103° |
perigee height: | 822 km |
apogee height: | 845 km |
right ascension of ascending node: | 32.0597° |
argument of perigee: | 267.8693° |
revolutions per day: | 14.17506084 |
mean anomaly at epoch: | 254.0848° |
orbit number at epoch: | 93553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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