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 24255.46317723 .00016389 00000-0 60150-3 0 9993
2 53807 53.2353 155.5526 0007923 13.1562 346.9644 15.28083917111412
Epoch (UTC): | 11 September 2024 11:06:58 |
Eccentricity: | 0.0007923 |
inclination: | 53.2353° |
perigee height: | 476 km |
apogee height: | 487 km |
right ascension of ascending node: | 155.5526° |
argument of perigee: | 13.1562° |
revolutions per day: | 15.28083917 |
mean anomaly at epoch: | 346.9644° |
orbit number at epoch: | 11141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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