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 66559U 26145.09283363 +.00000000 +00000-0 +56753-3 0 00005
2 66559 43.0024 275.6636 0001254 257.3539 102.7172 15.27579252 02
| Epoch (UTC): | 25 May 2026 02:13:40 |
| Eccentricity: | 0.0001254 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 275.6636° |
| argument of perigee: | 257.3539° |
| revolutions per day: | 15.27579252 |
| mean anomaly at epoch: | 102.7172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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