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 11267U 79011B 24311.43979716 .00002605 00000-0 26119-3 0 9997
2 11267 82.5269 199.4601 0014646 246.1233 113.8451 14.90919779477202
Epoch (UTC): | 06 November 2024 10:33:18 |
Eccentricity: | 0.0014646 |
inclination: | 82.5269° |
perigee height: | 585 km |
apogee height: | 605 km |
right ascension of ascending node: | 199.4601° |
argument of perigee: | 246.1233° |
revolutions per day: | 14.90919779 |
mean anomaly at epoch: | 113.8451° |
orbit number at epoch: | 47720 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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