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 26140.18961980 +.00000000 +00000-0 +76690-4 0 00005
2 22236 82.5051 210.5847 0012922 316.5847 43.4356 14.96454959 06
| Epoch (UTC): | 20 May 2026 04:33:03 |
| Eccentricity: | 0.0012922 |
| inclination: | 82.5051° |
| perigee height: | 569 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 210.5847° |
| argument of perigee: | 316.5847° |
| revolutions per day: | 14.96454959 |
| mean anomaly at epoch: | 43.4356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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