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 66426U 26145.46986016 +.00000000 +00000-0 +59288-3 0 00000
2 66426 43.0007 200.7577 0002491 288.6624 71.3957 15.27605550 08
| Epoch (UTC): | 25 May 2026 11:16:35 |
| Eccentricity: | 0.0002491 |
| inclination: | 43.0007° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 200.7577° |
| argument of perigee: | 288.6624° |
| revolutions per day: | 15.27605550 |
| mean anomaly at epoch: | 71.3957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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