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 67336U 26145.33216745 +.00000000 +00000-0 +46068-3 0 00004
2 67336 43.0012 154.3825 0001373 296.7545 63.3166 15.27589485 06
| Epoch (UTC): | 25 May 2026 07:58:19 |
| Eccentricity: | 0.0001373 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.3825° |
| argument of perigee: | 296.7545° |
| revolutions per day: | 15.27589485 |
| mean anomaly at epoch: | 63.3166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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