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 11870U 80056B 25196.91288068 .00000219 00000-0 80630-4 0 9994
2 11870 74.0514 185.9567 0014933 126.9316 233.3209 14.38210512334851
Epoch (UTC): | 15 July 2025 21:54:32 |
Eccentricity: | 0.0014933 |
inclination: | 74.0514° |
perigee height: | 754 km |
apogee height: | 775 km |
right ascension of ascending node: | 185.9567° |
argument of perigee: | 126.9316° |
revolutions per day: | 14.38210512 |
mean anomaly at epoch: | 233.3209° |
orbit number at epoch: | 33485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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