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 64250U 26145.30683002 +.00000000 +00000-0 +59811-3 0 00007
2 64250 43.0001 234.6415 0001576 246.7013 113.3673 15.27589951 00
| Epoch (UTC): | 25 May 2026 07:21:50 |
| Eccentricity: | 0.0001576 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 234.6415° |
| argument of perigee: | 246.7013° |
| revolutions per day: | 15.27589951 |
| mean anomaly at epoch: | 113.3673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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