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 67460U 26145.35413608 +.00000000 +00000-0 +56716-3 0 00002
2 67460 43.0045 132.5640 0002611 291.7128 68.3445 15.27601930 06
| Epoch (UTC): | 25 May 2026 08:29:57 |
| Eccentricity: | 0.0002611 |
| inclination: | 43.0045° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 132.5640° |
| argument of perigee: | 291.7128° |
| revolutions per day: | 15.27601930 |
| mean anomaly at epoch: | 68.3445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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