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 26101.80714344 +.00000000 +00000-0 +14607-3 0 00000
2 22236 82.5024 247.3482 0015653 82.6686 277.6314 14.96351688 05
| Epoch (UTC): | 11 April 2026 19:22:17 |
| Eccentricity: | 0.0015653 |
| inclination: | 82.5024° |
| perigee height: | 567 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 247.3482° |
| argument of perigee: | 82.6686° |
| revolutions per day: | 14.96351688 |
| mean anomaly at epoch: | 277.6314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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