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 67958U 26145.26870814 +.00000000 +00000-0 +58635-3 0 00002
2 67958 42.9997 118.1255 0001578 271.7818 88.2853 15.27593388 00
| Epoch (UTC): | 25 May 2026 06:26:56 |
| Eccentricity: | 0.0001578 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 118.1255° |
| argument of perigee: | 271.7818° |
| revolutions per day: | 15.27593388 |
| mean anomaly at epoch: | 88.2853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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