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 12139U 81003B 24311.44340134 .00027087 00000-0 91273-3 0 9991
2 12139 82.9397 14.5086 0341970 50.8748 312.2343 14.89381313241473
Epoch (UTC): | 06 November 2024 10:38:29 |
Eccentricity: | 0.0341970 |
inclination: | 82.9397° |
perigee height: | 361 km |
apogee height: | 838 km |
right ascension of ascending node: | 14.5086° |
argument of perigee: | 50.8748° |
revolutions per day: | 14.89381313 |
mean anomaly at epoch: | 312.2343° |
orbit number at epoch: | 24147 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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