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 26100.18226359 +.00000000 +00000-0 +43793-4 0 00004
2 22237 82.5146 0.8645 0020443 109.5631 250.7792 14.80341571 01
| Epoch (UTC): | 10 April 2026 04:22:27 |
| Eccentricity: | 0.0020443 |
| inclination: | 82.5146° |
| perigee height: | 614 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 0.8645° |
| argument of perigee: | 109.5631° |
| revolutions per day: | 14.80341571 |
| mean anomaly at epoch: | 250.7792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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