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 67362U 26145.31288750 +.00000000 +00000-0 +18014-3 0 00006
2 67362 42.9997 154.2283 0001469 268.2112 91.8571 15.27576012 00
| Epoch (UTC): | 25 May 2026 07:30:33 |
| Eccentricity: | 0.0001469 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.2283° |
| argument of perigee: | 268.2112° |
| revolutions per day: | 15.27576012 |
| mean anomaly at epoch: | 91.8571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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