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 39766U 26145.61742426 +.00000000 +00000-0 +66969-4 0 00004
2 39766 97.9221 243.1052 0001557 90.0997 270.0393 14.79465548 09
| Epoch (UTC): | 25 May 2026 14:49:05 |
| Eccentricity: | 0.0001557 |
| inclination: | 97.9221° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 243.1052° |
| argument of perigee: | 90.0997° |
| revolutions per day: | 14.79465548 |
| mean anomaly at epoch: | 270.0393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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