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 64472U 26145.62015484 +.00000000 +00000-0 +55277-3 0 00003
2 64472 53.1562 119.6908 0001117 83.6557 276.4570 15.30212513 09
| Epoch (UTC): | 25 May 2026 14:53:01 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.1562° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.6908° |
| argument of perigee: | 83.6557° |
| revolutions per day: | 15.30212513 |
| mean anomaly at epoch: | 276.4570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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