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 10967U 78064A 25191.36778428 .00000161 00000-0 83962-4 0 9991
2 10967 108.0100 337.1543 0000935 290.4939 69.6106 14.45862282471488
Epoch (UTC): | 10 July 2025 08:49:36 |
Eccentricity: | 0.0000935 |
inclination: | 108.0100° |
perigee height: | 738 km |
apogee height: | 740 km |
right ascension of ascending node: | 337.1543° |
argument of perigee: | 290.4939° |
revolutions per day: | 14.45862282 |
mean anomaly at epoch: | 69.6106° |
orbit number at epoch: | 47148 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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