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 43822U 26099.87360112 +.00000000 +00000-0 +26080-3 0 00005
2 43822 97.4395 151.5051 0006944 217.5574 142.5174 15.13947380 05
| Epoch (UTC): | 09 April 2026 20:57:59 |
| Eccentricity: | 0.0006944 |
| inclination: | 97.4395° |
| perigee height: | 519 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 151.5051° |
| argument of perigee: | 217.5574° |
| revolutions per day: | 15.13947380 |
| mean anomaly at epoch: | 142.5174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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