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 66504U 26145.10602563 +.00000000 +00000-0 +29345-3 0 00001
2 66504 42.9994 282.8167 0001394 265.2516 94.8177 15.27586310 02
| Epoch (UTC): | 25 May 2026 02:32:40 |
| Eccentricity: | 0.0001394 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 282.8167° |
| argument of perigee: | 265.2516° |
| revolutions per day: | 15.27586310 |
| mean anomaly at epoch: | 94.8177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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