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 17618U 81053KM 24357.63476976 .00004397 00000-0 24817-2 0 9996
2 17618 82.8477 211.9149 0053298 347.5878 66.9245 14.09350743 17609
Epoch (UTC): | 22 December 2024 15:14:04 |
Eccentricity: | 0.0053298 |
inclination: | 82.8477° |
perigee height: | 823 km |
apogee height: | 900 km |
right ascension of ascending node: | 211.9149° |
argument of perigee: | 347.5878° |
revolutions per day: | 14.09350743 |
mean anomaly at epoch: | 66.9245° |
orbit number at epoch: | 1760 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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