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 64456U 26145.54461116 +.00000000 +00000-0 +60864-3 0 00001
2 64456 53.1569 91.2816 0001314 82.6724 277.4426 15.30213080 06
| Epoch (UTC): | 25 May 2026 13:04:14 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1569° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.2816° |
| argument of perigee: | 82.6724° |
| revolutions per day: | 15.30213080 |
| mean anomaly at epoch: | 277.4426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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