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 26159.46119360 +.00000000 +00000-0 +44466-4 0 00000
2 22237 82.5109 305.5313 0017464 277.3211 82.6017 14.80372657 05
| Epoch (UTC): | 08 June 2026 11:04:07 |
| Eccentricity: | 0.0017464 |
| inclination: | 82.5109° |
| perigee height: | 616 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 305.5313° |
| argument of perigee: | 277.3211° |
| revolutions per day: | 14.80372657 |
| mean anomaly at epoch: | 82.6017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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