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 64080U 26145.39424696 +.00000000 +00000-0 +29488-3 0 00006
2 64080 43.0020 128.1670 0001454 272.2651 87.8034 15.27585979 01
| Epoch (UTC): | 25 May 2026 09:27:42 |
| Eccentricity: | 0.0001454 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 128.1670° |
| argument of perigee: | 272.2651° |
| revolutions per day: | 15.27585979 |
| mean anomaly at epoch: | 87.8034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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