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 67504U 26145.57636375 +.00000000 +00000-0 +50285-3 0 00008
2 67504 43.0029 239.9303 0001136 282.3592 77.7133 15.27594333 03
| Epoch (UTC): | 25 May 2026 13:49:57 |
| Eccentricity: | 0.0001136 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.9303° |
| argument of perigee: | 282.3592° |
| revolutions per day: | 15.27594333 |
| mean anomaly at epoch: | 77.7133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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