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 25348.88986668 .00000304 00000-0 17629-3 0 9993
2 16182 71.0035 319.0762 0006823 7.5277 12.5767 14.16585433 75225
| Epoch (UTC): | 14 December 2025 21:21:24 |
| Eccentricity: | 0.0006823 |
| inclination: | 71.0035° |
| perigee height: | 832 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 319.0762° |
| argument of perigee: | 7.5277° |
| revolutions per day: | 14.16585433 |
| mean anomaly at epoch: | 12.5767° |
| orbit number at epoch: | 7522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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