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 26106.52938421 +.00000000 +00000-0 +77563-5 0 00007
2 22161 62.9996 41.0756 0731649 234.8958 118.1359 13.32833169 04
| Epoch (UTC): | 16 April 2026 12:42:18 |
| Eccentricity: | 0.0731649 |
| inclination: | 62.9996° |
| perigee height: | 586 km |
| apogee height: | 1686 km |
| right ascension of ascending node: | 41.0756° |
| argument of perigee: | 234.8958° |
| revolutions per day: | 13.32833169 |
| mean anomaly at epoch: | 118.1359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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