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 5679U 71110B 25194.88242769 -.00000017 00000-0 29886-4 0 9990
2 5679 69.9980 350.2907 0013436 202.7226 157.3281 13.85632587322499
Epoch (UTC): | 13 July 2025 21:10:41 |
Eccentricity: | 0.0013436 |
inclination: | 69.9980° |
perigee height: | 934 km |
apogee height: | 954 km |
right ascension of ascending node: | 350.2907° |
argument of perigee: | 202.7226° |
revolutions per day: | 13.85632587 |
mean anomaly at epoch: | 157.3281° |
orbit number at epoch: | 32249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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