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 is defined by the following mean orbital elements,
1 18161U 26017.16585891 +.00000000 +00000-0 +10516-3 0 00005
2 18161 82.9317 257.5221 0031034 173.4282 357.1664 13.77412796 00
| Epoch (UTC): | 17 January 2026 03:58:50 |
| Eccentricity: | 0.0031034 |
| inclination: | 82.9317° |
| perigee height: | 950 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 257.5221° |
| argument of perigee: | 173.4282° |
| revolutions per day: | 13.77412796 |
| mean anomaly at epoch: | 357.1664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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