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 24316.18712699 .00019346 00000-0 66503-3 0 9995
2 53807 53.2340 234.4905 0008298 165.6971 194.4267 15.30106916120706
Epoch (UTC): | 11 November 2024 04:29:27 |
Eccentricity: | 0.0008298 |
inclination: | 53.2340° |
perigee height: | 470 km |
apogee height: | 481 km |
right ascension of ascending node: | 234.4905° |
argument of perigee: | 165.6971° |
revolutions per day: | 15.30106916 |
mean anomaly at epoch: | 194.4267° |
orbit number at epoch: | 12070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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