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 67459U 26145.36056278 +.00000000 +00000-0 +55465-3 0 00007
2 67459 43.0022 132.6050 0001647 249.8035 110.2640 15.27593919 05
| Epoch (UTC): | 25 May 2026 08:39:12 |
| Eccentricity: | 0.0001647 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.6050° |
| argument of perigee: | 249.8035° |
| revolutions per day: | 15.27593919 |
| mean anomaly at epoch: | 110.2640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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