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 64078U 26145.40452522 +.00000000 +00000-0 +60512-3 0 00007
2 64078 43.0031 128.2518 0002025 276.5147 83.5474 15.27592623 09
| Epoch (UTC): | 25 May 2026 09:42:30 |
| Eccentricity: | 0.0002025 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.2518° |
| argument of perigee: | 276.5147° |
| revolutions per day: | 15.27592623 |
| mean anomaly at epoch: | 83.5474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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