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 64266U 26145.37046139 +.00000000 +00000-0 +67029-3 0 00005
2 64266 53.1580 120.7081 0001217 73.0889 287.0245 15.30215821 09
| Epoch (UTC): | 25 May 2026 08:53:27 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 120.7081° |
| argument of perigee: | 73.0889° |
| revolutions per day: | 15.30215821 |
| mean anomaly at epoch: | 287.0245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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