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 67926U 26145.46321392 +.00000000 +00000-0 +24182-3 0 00001
2 67926 43.0027 171.6803 0001443 271.8056 88.2631 15.27588586 08
| Epoch (UTC): | 25 May 2026 11:07:01 |
| Eccentricity: | 0.0001443 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.6803° |
| argument of perigee: | 271.8056° |
| revolutions per day: | 15.27588586 |
| mean anomaly at epoch: | 88.2631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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