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 66446U 26145.48783625 +.00000000 +00000-0 +63466-3 0 00008
2 66446 43.0023 200.8823 0002067 287.7429 72.3197 15.27585313 06
| Epoch (UTC): | 25 May 2026 11:42:29 |
| Eccentricity: | 0.0002067 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.8823° |
| argument of perigee: | 287.7429° |
| revolutions per day: | 15.27585313 |
| mean anomaly at epoch: | 72.3197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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