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 22286U 26017.98978395 +.00000000 +00000-0 +15375-3 0 00001
2 22286 82.5189 285.8501 0019453 110.0834 250.2485 14.96921406 01
| Epoch (UTC): | 17 January 2026 23:45:17 |
| Eccentricity: | 0.0019453 |
| inclination: | 82.5189° |
| perigee height: | 563 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 285.8501° |
| argument of perigee: | 110.0834° |
| revolutions per day: | 14.96921406 |
| mean anomaly at epoch: | 250.2485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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