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 67494U 26145.53925375 +.00000000 +00000-0 +73087-3 0 00008
2 67494 43.0001 240.5397 0001525 273.9732 86.0945 15.27599577 05
| Epoch (UTC): | 25 May 2026 12:56:31 |
| Eccentricity: | 0.0001525 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.5397° |
| argument of perigee: | 273.9732° |
| revolutions per day: | 15.27599577 |
| mean anomaly at epoch: | 86.0945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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