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 64064U 26145.63559834 +.00000000 +00000-0 +21513-2 0 00008
2 64064 43.0008 354.9683 0002806 247.5217 112.5354 15.70999086 04
| Epoch (UTC): | 25 May 2026 15:15:15 |
| Eccentricity: | 0.0002806 |
| inclination: | 43.0008° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 354.9683° |
| argument of perigee: | 247.5217° |
| revolutions per day: | 15.70999086 |
| mean anomaly at epoch: | 112.5354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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