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 44311U 19032B 24358.21780700 .00019173 00000-0 90233-3 0 9996
2 44311 44.9760 58.8801 0008342 69.5776 290.5998 15.19295754305336
Epoch (UTC): | 23 December 2024 05:13:38 |
Eccentricity: | 0.0008342 |
inclination: | 44.9760° |
perigee height: | 502 km |
apogee height: | 514 km |
right ascension of ascending node: | 58.8801° |
argument of perigee: | 69.5776° |
revolutions per day: | 15.19295754 |
mean anomaly at epoch: | 290.5998° |
orbit number at epoch: | 30533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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