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 43181U 18014B 24358.18679731 .00006740 00000-0 29691-3 0 9992
2 43181 97.3883 262.8300 0001853 91.5112 268.6337 15.22145599382409
Epoch (UTC): | 23 December 2024 04:28:59 |
Eccentricity: | 0.0001853 |
inclination: | 97.3883° |
perigee height: | 498 km |
apogee height: | 500 km |
right ascension of ascending node: | 262.8300° |
argument of perigee: | 91.5112° |
revolutions per day: | 15.22145599 |
mean anomaly at epoch: | 268.6337° |
orbit number at epoch: | 38240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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