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 66566U 26145.39535091 +.00000000 +00000-0 +62918-3 0 00004
2 66566 42.9983 273.6304 0000862 192.3595 167.7236 15.27591951 08
| Epoch (UTC): | 25 May 2026 09:29:18 |
| Eccentricity: | 0.0000862 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.6304° |
| argument of perigee: | 192.3595° |
| revolutions per day: | 15.27591951 |
| mean anomaly at epoch: | 167.7236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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