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 42167U 81053SF 24352.59643879 .00001432 00000-0 12807-2 0 9994
2 42167 82.8380 100.6253 0055609 294.3663 65.1698 13.83102079557901
Epoch (UTC): | 17 December 2024 14:18:52 |
Eccentricity: | 0.0055609 |
inclination: | 82.8380° |
perigee height: | 912 km |
apogee height: | 993 km |
right ascension of ascending node: | 100.6253° |
argument of perigee: | 294.3663° |
revolutions per day: | 13.83102079 |
mean anomaly at epoch: | 65.1698° |
orbit number at epoch: | 55790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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