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 64086U 26145.42251780 +.00000000 +00000-0 +59812-3 0 00002
2 64086 43.0005 128.3791 0001190 258.6923 101.3795 15.27584529 09
| Epoch (UTC): | 25 May 2026 10:08:25 |
| Eccentricity: | 0.0001190 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.3791° |
| argument of perigee: | 258.6923° |
| revolutions per day: | 15.27584529 |
| mean anomaly at epoch: | 101.3795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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