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 66494U 26145.64372808 +.00000000 +00000-0 +10030-2 0 00004
2 66494 43.0005 276.4865 0001702 274.0234 86.0423 15.27602179 06
| Epoch (UTC): | 25 May 2026 15:26:58 |
| Eccentricity: | 0.0001702 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 276.4865° |
| argument of perigee: | 274.0234° |
| revolutions per day: | 15.27602179 |
| mean anomaly at epoch: | 86.0423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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