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 46746U 26145.58335647 +.00000000 +00000-0 +58755-3 0 00002
2 46746 53.0364 262.4930 0005425 293.3379 345.8481 15.80497138 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005425 |
| inclination: | 53.0364° |
| perigee height: | 325 km |
| apogee height: | 333 km |
| right ascension of ascending node: | 262.4930° |
| argument of perigee: | 293.3379° |
| revolutions per day: | 15.80497138 |
| mean anomaly at epoch: | 345.8481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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