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 43566U 26142.10926412 +.00000000 +00000-0 +00000-0 0 00007
2 43566 57.1804 342.4893 0002684 333.4673 26.5384 1.70475765 03
| Epoch (UTC): | 22 May 2026 02:37:20 |
| Eccentricity: | 0.0002684 |
| inclination: | 57.1804° |
| perigee height: | 23214 km |
| apogee height: | 23230 km |
| right ascension of ascending node: | 342.4893° |
| argument of perigee: | 333.4673° |
| revolutions per day: | 1.70475765 |
| mean anomaly at epoch: | 26.5384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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