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 54511U 22151JP 25194.18885653 .00000152 00000-0 13608-3 0 9991
2 54511 98.8635 171.2500 0129881 304.8441 54.0561 13.94559278135458
Epoch (UTC): | 13 July 2025 04:31:57 |
Eccentricity: | 0.0129881 |
inclination: | 98.8635° |
perigee height: | 818 km |
apogee height: | 1007 km |
right ascension of ascending node: | 171.2500° |
argument of perigee: | 304.8441° |
revolutions per day: | 13.94559278 |
mean anomaly at epoch: | 54.0561° |
orbit number at epoch: | 13545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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