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 66613U 26145.57269780 +.00000000 +00000-0 +60431-3 0 00004
2 66613 43.0043 342.0352 0000685 231.0545 129.0246 15.27585009 02
| Epoch (UTC): | 25 May 2026 13:44:41 |
| Eccentricity: | 0.0000685 |
| inclination: | 43.0043° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.0352° |
| argument of perigee: | 231.0545° |
| revolutions per day: | 15.27585009 |
| mean anomaly at epoch: | 129.0246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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