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 66366U 26145.22902718 +.00000000 +00000-0 +28789-2 0 00005
2 66366 53.1586 236.9737 0003240 312.0719 48.0006 15.30376800 07
| Epoch (UTC): | 25 May 2026 05:29:47 |
| Eccentricity: | 0.0003240 |
| inclination: | 53.1586° |
| perigee height: | 472 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 236.9737° |
| argument of perigee: | 312.0719° |
| revolutions per day: | 15.30376800 |
| mean anomaly at epoch: | 48.0006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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