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 64688U 26145.22497747 +.00000000 +00000-0 +76544-3 0 00004
2 64688 53.1591 130.7089 0001009 48.9071 311.2019 15.34397600 00
| Epoch (UTC): | 25 May 2026 05:23:58 |
| Eccentricity: | 0.0001009 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.7089° |
| argument of perigee: | 48.9071° |
| revolutions per day: | 15.34397600 |
| mean anomaly at epoch: | 311.2019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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