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 16182U 85097B 25198.49482016 .00000086 00000-0 67315-4 0 9996
2 16182 71.0026 275.6870 0009658 258.3437 188.9582 14.16554593 54239
Epoch (UTC): | 17 July 2025 11:52:32 |
Eccentricity: | 0.0009658 |
inclination: | 71.0026° |
perigee height: | 830 km |
apogee height: | 844 km |
right ascension of ascending node: | 275.6870° |
argument of perigee: | 258.3437° |
revolutions per day: | 14.16554593 |
mean anomaly at epoch: | 188.9582° |
orbit number at epoch: | 5423 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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