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 64486U 26145.61909985 +.00000000 +00000-0 +63883-3 0 00007
2 64486 53.1566 119.6788 0001376 86.8006 273.3152 15.30212594 06
| Epoch (UTC): | 25 May 2026 14:51:30 |
| Eccentricity: | 0.0001376 |
| inclination: | 53.1566° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.6788° |
| argument of perigee: | 86.8006° |
| revolutions per day: | 15.30212594 |
| mean anomaly at epoch: | 273.3152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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