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 66267U 26145.39354382 +.00000000 +00000-0 +47027-3 0 00008
2 66267 53.1593 193.9668 0001418 45.0589 315.0529 15.34399140 06
| Epoch (UTC): | 25 May 2026 09:26:42 |
| Eccentricity: | 0.0001418 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 193.9668° |
| argument of perigee: | 45.0589° |
| revolutions per day: | 15.34399140 |
| mean anomaly at epoch: | 315.0529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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