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 11267U 79011B 25197.05998153 .00000500 00000-0 47269-4 0 9996
2 11267 82.5261 320.9842 0017390 125.0126 235.2729 14.91516546514707
Epoch (UTC): | 16 July 2025 01:26:22 |
Eccentricity: | 0.0017390 |
inclination: | 82.5261° |
perigee height: | 581 km |
apogee height: | 605 km |
right ascension of ascending node: | 320.9842° |
argument of perigee: | 125.0126° |
revolutions per day: | 14.91516546 |
mean anomaly at epoch: | 235.2729° |
orbit number at epoch: | 51470 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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