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 67925U 26145.46706711 +.00000000 +00000-0 +28008-3 0 00003
2 67925 43.0037 171.7180 0001748 252.0090 108.0571 15.27583685 03
| Epoch (UTC): | 25 May 2026 11:12:34 |
| Eccentricity: | 0.0001748 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.7180° |
| argument of perigee: | 252.0090° |
| revolutions per day: | 15.27583685 |
| mean anomaly at epoch: | 108.0571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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