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 67354U 26145.06419653 +.00000000 +00000-0 +22966-3 0 00008
2 67354 43.0007 155.8088 0000621 271.4296 88.6485 15.27593280 07
| Epoch (UTC): | 25 May 2026 01:32:26 |
| Eccentricity: | 0.0000621 |
| inclination: | 43.0007° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 155.8088° |
| argument of perigee: | 271.4296° |
| revolutions per day: | 15.27593280 |
| mean anomaly at epoch: | 88.6485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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