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 66576U 26145.35568404 +.00000000 +00000-0 +11674-2 0 00007
2 66576 43.0039 274.2001 0001775 284.8790 75.1865 15.27602364 03
| Epoch (UTC): | 25 May 2026 08:32:11 |
| Eccentricity: | 0.0001775 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.2001° |
| argument of perigee: | 284.8790° |
| revolutions per day: | 15.27602364 |
| mean anomaly at epoch: | 75.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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