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 67166U 26145.56272487 +.00000000 +00000-0 +53937-3 0 00008
2 67166 42.9998 236.4305 0001159 273.5360 86.5359 15.27595884 04
| Epoch (UTC): | 25 May 2026 13:30:19 |
| Eccentricity: | 0.0001159 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.4305° |
| argument of perigee: | 273.5360° |
| revolutions per day: | 15.27595884 |
| mean anomaly at epoch: | 86.5359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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