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 67626U 26145.50067310 +.00000000 +00000-0 +44320-3 0 00006
2 67626 43.0053 65.7435 0001224 270.6165 89.4547 15.27593266 03
| Epoch (UTC): | 25 May 2026 12:00:58 |
| Eccentricity: | 0.0001224 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.7435° |
| argument of perigee: | 270.6165° |
| revolutions per day: | 15.27593266 |
| mean anomaly at epoch: | 89.4547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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