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 66849U 26145.65230522 +.00000000 +00000-0 +56183-3 0 00005
2 66849 42.9980 269.0333 0000961 283.0521 77.0223 15.27599041 04
| Epoch (UTC): | 25 May 2026 15:39:19 |
| Eccentricity: | 0.0000961 |
| inclination: | 42.9980° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 269.0333° |
| argument of perigee: | 283.0521° |
| revolutions per day: | 15.27599041 |
| mean anomaly at epoch: | 77.0223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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