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 26039.60458604 +.00000000 +00000-0 +53262-4 0 00005
2 18422 82.5092 94.5660 0020235 105.9347 254.4101 14.85301134 03
| Epoch (UTC): | 08 February 2026 14:30:36 |
| Eccentricity: | 0.0020235 |
| inclination: | 82.5092° |
| perigee height: | 598 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 94.5660° |
| argument of perigee: | 105.9347° |
| revolutions per day: | 14.85301134 |
| mean anomaly at epoch: | 254.4101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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