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 66804U 26145.40386215 +.00000000 +00000-0 +52969-3 0 00008
2 66804 42.9969 40.9468 0001631 277.7535 82.3131 15.27589930 00
| Epoch (UTC): | 25 May 2026 09:41:33 |
| Eccentricity: | 0.0001631 |
| inclination: | 42.9969° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.9468° |
| argument of perigee: | 277.7535° |
| revolutions per day: | 15.27589930 |
| mean anomaly at epoch: | 82.3131° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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