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 36834U 10038A 24358.14857869 .00001635 00000-0 20448-3 0 9992
2 36834 97.9385 14.2239 0001608 87.0919 312.9966 14.83662773777012
Epoch (UTC): | 23 December 2024 03:33:57 |
Eccentricity: | 0.0001608 |
inclination: | 97.9385° |
perigee height: | 616 km |
apogee height: | 619 km |
right ascension of ascending node: | 14.2239° |
argument of perigee: | 87.0919° |
revolutions per day: | 14.83662773 |
mean anomaly at epoch: | 312.9966° |
orbit number at epoch: | 77701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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