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 67042U 26145.54933375 +.00000000 +00000-0 +72664-3 0 00007
2 67042 42.9997 324.0372 0001173 255.7880 104.2841 15.27590966 09
| Epoch (UTC): | 25 May 2026 13:11:02 |
| Eccentricity: | 0.0001173 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.0372° |
| argument of perigee: | 255.7880° |
| revolutions per day: | 15.27590966 |
| mean anomaly at epoch: | 104.2841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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