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 37841U 11058D 25197.65894075 .00000362 00000-0 52711-4 0 9997
2 37841 19.9723 290.1716 0011850 112.1624 37.5320 14.11444655710355
Epoch (UTC): | 16 July 2025 15:48:52 |
Eccentricity: | 0.0011850 |
inclination: | 19.9723° |
perigee height: | 846 km |
apogee height: | 863 km |
right ascension of ascending node: | 290.1716° |
argument of perigee: | 112.1624° |
revolutions per day: | 14.11444655 |
mean anomaly at epoch: | 37.5320° |
orbit number at epoch: | 71035 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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