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 22236U 26139.58782328 +.00000000 +00000-0 +71979-4 0 00009
2 22236 82.5052 211.1610 0012966 318.7723 41.2519 14.96453546 05
| Epoch (UTC): | 19 May 2026 14:06:27 |
| Eccentricity: | 0.0012966 |
| inclination: | 82.5052° |
| perigee height: | 569 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 211.1610° |
| argument of perigee: | 318.7723° |
| revolutions per day: | 14.96453546 |
| mean anomaly at epoch: | 41.2519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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