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 67930U 26145.37598060 +.00000000 +00000-0 +51654-3 0 00008
2 67930 43.0012 171.8737 0001426 278.6462 81.4228 15.27581394 09
| Epoch (UTC): | 25 May 2026 09:01:24 |
| Eccentricity: | 0.0001426 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.8737° |
| argument of perigee: | 278.6462° |
| revolutions per day: | 15.27581394 |
| mean anomaly at epoch: | 81.4228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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