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 67464U 26145.43737992 +.00000000 +00000-0 +44435-3 0 00005
2 67464 43.0024 131.4584 0001897 270.2393 89.8241 15.27572277 06
| Epoch (UTC): | 25 May 2026 10:29:49 |
| Eccentricity: | 0.0001897 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 131.4584° |
| argument of perigee: | 270.2393° |
| revolutions per day: | 15.27572277 |
| mean anomaly at epoch: | 89.8241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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