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 67746U 26145.34917640 +.00000000 +00000-0 +28510-3 0 00004
2 67746 97.5030 273.6882 0008450 297.7437 62.2939 15.18807624 01
| Epoch (UTC): | 25 May 2026 08:22:48 |
| Eccentricity: | 0.0008450 |
| inclination: | 97.5030° |
| perigee height: | 504 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 273.6882° |
| argument of perigee: | 297.7437° |
| revolutions per day: | 15.18807624 |
| mean anomaly at epoch: | 62.2939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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