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 67935U 26145.62391669 +.00000000 +00000-0 +60651-3 0 00004
2 67935 42.9986 116.5231 0001032 271.5967 88.4766 15.27595134 03
| Epoch (UTC): | 25 May 2026 14:58:26 |
| Eccentricity: | 0.0001032 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.5231° |
| argument of perigee: | 271.5967° |
| revolutions per day: | 15.27595134 |
| mean anomaly at epoch: | 88.4766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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