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 67471U 26145.36184333 +.00000000 +00000-0 +42590-3 0 00000
2 67471 43.0024 132.6054 0002051 286.2779 73.7847 15.27587627 06
| Epoch (UTC): | 25 May 2026 08:41:03 |
| Eccentricity: | 0.0002051 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.6054° |
| argument of perigee: | 286.2779° |
| revolutions per day: | 15.27587627 |
| mean anomaly at epoch: | 73.7847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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