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 64257U 26145.61800389 +.00000000 +00000-0 +10062-2 0 00001
2 64257 53.1571 119.4089 0001191 80.9093 279.2042 15.30206851 08
| Epoch (UTC): | 25 May 2026 14:49:55 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1571° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 119.4089° |
| argument of perigee: | 80.9093° |
| revolutions per day: | 15.30206851 |
| mean anomaly at epoch: | 279.2042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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