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 66456U 26145.52487549 +.00000000 +00000-0 +57530-3 0 00005
2 66456 43.0030 222.5746 0002058 280.7601 79.3019 15.27585986 01
| Epoch (UTC): | 25 May 2026 12:35:49 |
| Eccentricity: | 0.0002058 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.5746° |
| argument of perigee: | 280.7601° |
| revolutions per day: | 15.27585986 |
| mean anomaly at epoch: | 79.3019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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