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 23705U 95058B 25193.78273229 -.00000242 00000-0 -99532-4 0 9996
2 23705 71.0226 323.9194 0010810 132.3112 227.8929 14.15451258533906
Epoch (UTC): | 12 July 2025 18:47:08 |
Eccentricity: | 0.0010810 |
inclination: | 71.0226° |
perigee height: | 833 km |
apogee height: | 848 km |
right ascension of ascending node: | 323.9194° |
argument of perigee: | 132.3112° |
revolutions per day: | 14.15451258 |
mean anomaly at epoch: | 227.8929° |
orbit number at epoch: | 53390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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