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 67426U 26145.52956115 +.00000000 +00000-0 +94838-3 0 00005
2 67426 43.0006 164.4180 0003844 241.3029 118.7437 15.27636095 09
| Epoch (UTC): | 25 May 2026 12:42:34 |
| Eccentricity: | 0.0003844 |
| inclination: | 43.0006° |
| perigee height: | 480 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 164.4180° |
| argument of perigee: | 241.3029° |
| revolutions per day: | 15.27636095 |
| mean anomaly at epoch: | 118.7437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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