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 53807U 22111AL 24308.60939057 .00018865 00000-0 65510-3 0 9994
2 53807 53.2347 269.6136 0008510 143.1320 217.0268 15.29792207119540
Epoch (UTC): | 03 November 2024 14:37:31 |
Eccentricity: | 0.0008510 |
inclination: | 53.2347° |
perigee height: | 470 km |
apogee height: | 482 km |
right ascension of ascending node: | 269.6136° |
argument of perigee: | 143.1320° |
revolutions per day: | 15.29792207 |
mean anomaly at epoch: | 217.0268° |
orbit number at epoch: | 11954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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