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 25194.54136765 -.00000143 00000-0 -47727-4 0 9996
2 16182 71.0033 284.0093 0009752 263.1524 189.1739 14.16554449 53364
Epoch (UTC): | 13 July 2025 12:59:34 |
Eccentricity: | 0.0009752 |
inclination: | 71.0033° |
perigee height: | 830 km |
apogee height: | 844 km |
right ascension of ascending node: | 284.0093° |
argument of perigee: | 263.1524° |
revolutions per day: | 14.16554449 |
mean anomaly at epoch: | 189.1739° |
orbit number at epoch: | 5336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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