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 15055U 84062A 23338.11910712 .00000097 00000-0 86169-4 0 9997
2 15055 82.9591 42.2173 0028647 112.4950 259.4566 13.74414876978545
Epoch (UTC): | 04 December 2023 02:51:30 |
Eccentricity: | 0.0028647 |
inclination: | 82.9591° |
perigee height: | 962 km |
apogee height: | 1005 km |
right ascension of ascending node: | 42.2173° |
argument of perigee: | 112.4950° |
revolutions per day: | 13.74414876 |
mean anomaly at epoch: | 259.4566° |
orbit number at epoch: | 97854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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