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 67938U 26145.61363748 +.00000000 +00000-0 +27365-3 0 00008
2 67938 42.9980 116.4388 0000838 257.4529 102.6229 15.27601717 00
| Epoch (UTC): | 25 May 2026 14:43:38 |
| Eccentricity: | 0.0000838 |
| inclination: | 42.9980° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.4388° |
| argument of perigee: | 257.4529° |
| revolutions per day: | 15.27601717 |
| mean anomaly at epoch: | 102.6229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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