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 25199.18583944 .00000215 00000-0 99131-4 0 9991
2 10967 108.0113 353.5498 0001138 298.8769 61.2262 14.45867796472928
Epoch (UTC): | 18 July 2025 04:27:36 |
Eccentricity: | 0.0001138 |
inclination: | 108.0113° |
perigee height: | 738 km |
apogee height: | 740 km |
right ascension of ascending node: | 353.5498° |
argument of perigee: | 298.8769° |
revolutions per day: | 14.45867796 |
mean anomaly at epoch: | 61.2262° |
orbit number at epoch: | 47292 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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