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 64537U 26145.56611860 +.00000000 +00000-0 +88315-3 0 00007
2 64537 97.4695 261.2130 0001730 229.3929 130.7157 15.22710919 00
| Epoch (UTC): | 25 May 2026 13:35:12 |
| Eccentricity: | 0.0001730 |
| inclination: | 97.4695° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 261.2130° |
| argument of perigee: | 229.3929° |
| revolutions per day: | 15.22710919 |
| mean anomaly at epoch: | 130.7157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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