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 67428U 26145.43077477 +.00000000 +00000-0 +41967-3 0 00007
2 67428 43.0026 164.5313 0001350 267.1534 92.9163 15.27591178 00
| Epoch (UTC): | 25 May 2026 10:20:18 |
| Eccentricity: | 0.0001350 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.5313° |
| argument of perigee: | 267.1534° |
| revolutions per day: | 15.27591178 |
| mean anomaly at epoch: | 92.9163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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