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 67339U 26145.32832858 +.00000000 +00000-0 +76954-3 0 00002
2 67339 42.9998 154.3532 0001008 276.4334 83.6403 15.27608750 07
| Epoch (UTC): | 25 May 2026 07:52:47 |
| Eccentricity: | 0.0001008 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.3532° |
| argument of perigee: | 276.4334° |
| revolutions per day: | 15.27608750 |
| mean anomaly at epoch: | 83.6403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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