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 22161U 26104.12852829 +.00000000 +00000-0 +89159-5 0 00002
2 22161 62.9990 47.2593 0731782 234.6765 118.3718 13.32833092 03
| Epoch (UTC): | 14 April 2026 03:05:04 |
| Eccentricity: | 0.0731782 |
| inclination: | 62.9990° |
| perigee height: | 586 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 47.2593° |
| argument of perigee: | 234.6765° |
| revolutions per day: | 13.32833092 |
| mean anomaly at epoch: | 118.3718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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