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 41512U 00055ML 24357.90973869 .00019430 00000-0 56808-2 0 9991
2 41512 98.9633 162.6726 0035321 237.1443 122.6344 14.43650505455864
Epoch (UTC): | 22 December 2024 21:50:01 |
Eccentricity: | 0.0035321 |
inclination: | 98.9633° |
perigee height: | 721 km |
apogee height: | 771 km |
right ascension of ascending node: | 162.6726° |
argument of perigee: | 237.1443° |
revolutions per day: | 14.43650505 |
mean anomaly at epoch: | 122.6344° |
orbit number at epoch: | 45586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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