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 26053.71013887 +.00000000 +00000-0 +24133-3 0 00002
2 22161 62.9972 177.1302 0734483 230.0493 123.3766 13.32800001 06
| Epoch (UTC): | 22 February 2026 17:02:35 |
| Eccentricity: | 0.0734483 |
| inclination: | 62.9972° |
| perigee height: | 584 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 177.1302° |
| argument of perigee: | 230.0493° |
| revolutions per day: | 13.32800001 |
| mean anomaly at epoch: | 123.3766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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