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 67411U 26145.36153153 +.00000000 +00000-0 +29011-3 0 00003
2 67411 43.0020 164.8733 0001261 261.8814 98.1895 15.27581168 06
| Epoch (UTC): | 25 May 2026 08:40:36 |
| Eccentricity: | 0.0001261 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.8733° |
| argument of perigee: | 261.8814° |
| revolutions per day: | 15.27581168 |
| mean anomaly at epoch: | 98.1895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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