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 64826U 26145.47396498 +.00000000 +00000-0 +45525-3 0 00001
2 64826 51.9002 321.0174 0000664 105.4444 254.6592 14.79933827 07
| Epoch (UTC): | 25 May 2026 11:22:30 |
| Eccentricity: | 0.0000664 |
| inclination: | 51.9002° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 321.0174° |
| argument of perigee: | 105.4444° |
| revolutions per day: | 14.79933827 |
| mean anomaly at epoch: | 254.6592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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