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 67337U 26145.41555469 +.00000000 +00000-0 +72347-3 0 00002
2 67337 43.0010 154.1558 0000762 248.3012 111.7759 15.27589845 05
| Epoch (UTC): | 25 May 2026 09:58:23 |
| Eccentricity: | 0.0000762 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.1558° |
| argument of perigee: | 248.3012° |
| revolutions per day: | 15.27589845 |
| mean anomaly at epoch: | 111.7759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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