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 66126U 26145.43128397 +.00000000 +00000-0 +83166-3 0 00006
2 66126 53.1605 42.9046 0001998 86.9794 273.1435 15.30202781 02
| Epoch (UTC): | 25 May 2026 10:21:02 |
| Eccentricity: | 0.0001998 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 42.9046° |
| argument of perigee: | 86.9794° |
| revolutions per day: | 15.30202781 |
| mean anomaly at epoch: | 273.1435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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