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 64589U 26145.59623650 +.00000000 +00000-0 +18296-3 0 00008
2 64589 97.7692 260.3577 0006074 60.3122 299.8702 14.94226106 07
| Epoch (UTC): | 25 May 2026 14:18:34 |
| Eccentricity: | 0.0006074 |
| inclination: | 97.7692° |
| perigee height: | 581 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 260.3577° |
| argument of perigee: | 60.3122° |
| revolutions per day: | 14.94226106 |
| mean anomaly at epoch: | 299.8702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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