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 67456U 26145.32072970 +.00000000 +00000-0 +26141-3 0 00006
2 67456 42.9974 132.3055 0001459 273.2366 86.8318 15.27585686 09
| Epoch (UTC): | 25 May 2026 07:41:51 |
| Eccentricity: | 0.0001459 |
| inclination: | 42.9974° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.3055° |
| argument of perigee: | 273.2366° |
| revolutions per day: | 15.27585686 |
| mean anomaly at epoch: | 86.8318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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