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 66498U 26145.43343869 +.00000000 +00000-0 +92789-3 0 00002
2 66498 43.0021 277.4876 0001272 250.4198 109.6517 15.27594289 08
| Epoch (UTC): | 25 May 2026 10:24:09 |
| Eccentricity: | 0.0001272 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.4876° |
| argument of perigee: | 250.4198° |
| revolutions per day: | 15.27594289 |
| mean anomaly at epoch: | 109.6517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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