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 64327U 26145.66261256 +.00000000 +00000-0 +18784-2 0 00007
2 64327 43.0005 284.9381 0000787 190.2797 169.8054 15.70865046 03
| Epoch (UTC): | 25 May 2026 15:54:09 |
| Eccentricity: | 0.0000787 |
| inclination: | 43.0005° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 284.9381° |
| argument of perigee: | 190.2797° |
| revolutions per day: | 15.70865046 |
| mean anomaly at epoch: | 169.8054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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