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 18422U 26040.68247522 +.00000000 +00000-0 +53931-4 0 00003
2 18422 82.5090 93.5518 0020264 102.6381 257.7102 14.85302263 07
| Epoch (UTC): | 09 February 2026 16:22:45 |
| Eccentricity: | 0.0020264 |
| inclination: | 82.5090° |
| perigee height: | 598 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 93.5518° |
| argument of perigee: | 102.6381° |
| revolutions per day: | 14.85302263 |
| mean anomaly at epoch: | 257.7102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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