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 22006U 26053.73479839 +.00000000 +00000-0 +55919-4 0 00002
2 22006 82.9374 143.0746 0035993 232.1008 240.9792 13.75181572 08
| Epoch (UTC): | 22 February 2026 17:38:06 |
| Eccentricity: | 0.0035993 |
| inclination: | 82.9374° |
| perigee height: | 955 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 143.0746° |
| argument of perigee: | 232.1008° |
| revolutions per day: | 13.75181572 |
| mean anomaly at epoch: | 240.9792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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