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 67418U 26145.43463321 +.00000000 +00000-0 +52260-3 0 00001
2 67418 43.0037 164.5636 0001672 275.8664 84.1997 15.27580762 01
| Epoch (UTC): | 25 May 2026 10:25:52 |
| Eccentricity: | 0.0001672 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5636° |
| argument of perigee: | 275.8664° |
| revolutions per day: | 15.27580762 |
| mean anomaly at epoch: | 84.1997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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