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 18637U 81053LX 23027.36227237 .00004853 00000-0 26220-2 0 9992
2 18637 82.9711 167.3156 0060969 244.2393 115.2484 14.11502793921843
Epoch (UTC): | 27 January 2023 08:41:40 |
Eccentricity: | 0.0060969 |
inclination: | 82.9711° |
perigee height: | 810 km |
apogee height: | 898 km |
right ascension of ascending node: | 167.3156° |
argument of perigee: | 244.2393° |
revolutions per day: | 14.11502793 |
mean anomaly at epoch: | 115.2484° |
orbit number at epoch: | 92184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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