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 24317.49348193 .00014365 00000-0 49670-3 0 9996
2 53807 53.2351 228.4337 0008196 169.0309 191.0873 15.30146121120900
Epoch (UTC): | 12 November 2024 11:50:36 |
Eccentricity: | 0.0008196 |
inclination: | 53.2351° |
perigee height: | 470 km |
apogee height: | 481 km |
right ascension of ascending node: | 228.4337° |
argument of perigee: | 169.0309° |
revolutions per day: | 15.30146121 |
mean anomaly at epoch: | 191.0873° |
orbit number at epoch: | 12090 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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