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 67359U 26145.35272731 +.00000000 +00000-0 +71224-3 0 00000
2 67359 43.0037 154.5367 0001836 246.5087 113.5572 15.27581806 07
| Epoch (UTC): | 25 May 2026 08:27:55 |
| Eccentricity: | 0.0001836 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.5367° |
| argument of perigee: | 246.5087° |
| revolutions per day: | 15.27581806 |
| mean anomaly at epoch: | 113.5572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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