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 67445U 26145.35285833 +.00000000 +00000-0 +56600-3 0 00004
2 67445 43.0021 132.5585 0001371 268.5816 91.4879 15.27593497 05
| Epoch (UTC): | 25 May 2026 08:28:06 |
| Eccentricity: | 0.0001371 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.5585° |
| argument of perigee: | 268.5816° |
| revolutions per day: | 15.27593497 |
| mean anomaly at epoch: | 91.4879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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