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 64264U 26145.32484404 +.00000000 +00000-0 +80889-3 0 00008
2 64264 53.1611 118.2976 0001145 83.5088 276.6045 15.35427958 07
| Epoch (UTC): | 25 May 2026 07:47:46 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1611° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 118.2976° |
| argument of perigee: | 83.5088° |
| revolutions per day: | 15.35427958 |
| mean anomaly at epoch: | 276.6045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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