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 64461U 26145.26130617 +.00000000 +00000-0 +10322-2 0 00008
2 64461 53.1590 93.0669 0001586 73.5799 286.5376 15.30205826 08
| Epoch (UTC): | 25 May 2026 06:16:16 |
| Eccentricity: | 0.0001586 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 93.0669° |
| argument of perigee: | 73.5799° |
| revolutions per day: | 15.30205826 |
| mean anomaly at epoch: | 286.5376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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