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 25192.40382019 .00003555 00000-0 12007-3 0 9997
2 53807 53.2300 188.1233 0006423 196.0824 163.9976 15.33370368157833
Epoch (UTC): | 11 July 2025 09:41:30 |
Eccentricity: | 0.0006423 |
inclination: | 53.2300° |
perigee height: | 461 km |
apogee height: | 470 km |
right ascension of ascending node: | 188.1233° |
argument of perigee: | 196.0824° |
revolutions per day: | 15.33370368 |
mean anomaly at epoch: | 163.9976° |
orbit number at epoch: | 15783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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