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 26042.09720338 +.00000000 +00000-0 +49955-4 0 00002
2 18422 82.5088 92.2207 0020289 98.3101 262.0417 14.85303521 09
| Epoch (UTC): | 11 February 2026 02:19:58 |
| Eccentricity: | 0.0020289 |
| inclination: | 82.5088° |
| perigee height: | 598 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 92.2207° |
| argument of perigee: | 98.3101° |
| revolutions per day: | 14.85303521 |
| mean anomaly at epoch: | 262.0417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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