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 22237U 26108.63145583 +.00000000 +00000-0 +27348-4 0 00009
2 22237 82.5135 352.9811 0020550 83.9279 276.4275 14.80344672 03
| Epoch (UTC): | 18 April 2026 15:09:17 |
| Eccentricity: | 0.0020550 |
| inclination: | 82.5135° |
| perigee height: | 614 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 352.9811° |
| argument of perigee: | 83.9279° |
| revolutions per day: | 14.80344672 |
| mean anomaly at epoch: | 276.4275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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