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 66450U 26145.42116568 +.00000000 +00000-0 +66165-3 0 00002
2 66450 43.0008 201.2403 0001627 290.5456 69.5221 15.27591021 05
| Epoch (UTC): | 25 May 2026 10:06:28 |
| Eccentricity: | 0.0001627 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 201.2403° |
| argument of perigee: | 290.5456° |
| revolutions per day: | 15.27591021 |
| mean anomaly at epoch: | 69.5221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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