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 66179U 26145.57730576 +.00000000 +00000-0 +25567-3 0 00008
2 66179 53.1584 248.2524 0000582 352.6157 7.4836 15.30207751 07
| Epoch (UTC): | 25 May 2026 13:51:19 |
| Eccentricity: | 0.0000582 |
| inclination: | 53.1584° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2524° |
| argument of perigee: | 352.6157° |
| revolutions per day: | 15.30207751 |
| mean anomaly at epoch: | 7.4836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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