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 67644U 26145.49682016 +.00000000 +00000-0 +48277-3 0 00005
2 67644 43.0041 65.7120 0000794 276.5207 83.5554 15.27590387 08
| Epoch (UTC): | 25 May 2026 11:55:25 |
| Eccentricity: | 0.0000794 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.7120° |
| argument of perigee: | 276.5207° |
| revolutions per day: | 15.27590387 |
| mean anomaly at epoch: | 83.5554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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