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 64331U 26145.01966344 +.00000000 +00000-0 +53712-3 0 00002
2 64331 42.9998 50.6742 0001613 275.8855 84.1813 15.27593742 05
| Epoch (UTC): | 25 May 2026 00:28:18 |
| Eccentricity: | 0.0001613 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 50.6742° |
| argument of perigee: | 275.8855° |
| revolutions per day: | 15.27593742 |
| mean anomaly at epoch: | 84.1813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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