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 67338U 26145.34245734 +.00000000 +00000-0 +45092-3 0 00003
2 67338 43.0021 154.4673 0001417 271.1374 88.9315 15.27587655 02
| Epoch (UTC): | 25 May 2026 08:13:08 |
| Eccentricity: | 0.0001417 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.4673° |
| argument of perigee: | 271.1374° |
| revolutions per day: | 15.27587655 |
| mean anomaly at epoch: | 88.9315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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