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 42131U 81053QT 24279.39022168 .00045155 00000-0 13345-1 0 9990
2 42131 82.8759 153.5182 0021261 26.6404 98.7303 14.43080504565264
Epoch (UTC): | 05 October 2024 09:21:55 |
Eccentricity: | 0.0021261 |
inclination: | 82.8759° |
perigee height: | 733 km |
apogee height: | 763 km |
right ascension of ascending node: | 153.5182° |
argument of perigee: | 26.6404° |
revolutions per day: | 14.43080504 |
mean anomaly at epoch: | 98.7303° |
orbit number at epoch: | 56526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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