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 67430U 26145.51157950 +.00000000 +00000-0 +50347-3 0 00006
2 67430 43.0034 164.2849 0001873 264.3629 95.7009 15.27597254 08
| Epoch (UTC): | 25 May 2026 12:16:40 |
| Eccentricity: | 0.0001873 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.2849° |
| argument of perigee: | 264.3629° |
| revolutions per day: | 15.27597254 |
| mean anomaly at epoch: | 95.7009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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