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 19650U 88102B 25196.70905949 .00000062 00000-0 55560-4 0 9999
2 19650 71.0006 290.1073 0014047 2.4883 357.6308 14.16110390893345
Epoch (UTC): | 15 July 2025 17:01:02 |
Eccentricity: | 0.0014047 |
inclination: | 71.0006° |
perigee height: | 828 km |
apogee height: | 848 km |
right ascension of ascending node: | 290.1073° |
argument of perigee: | 2.4883° |
revolutions per day: | 14.16110390 |
mean anomaly at epoch: | 357.6308° |
orbit number at epoch: | 89334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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