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 67347U 26145.32959595 +.00000000 +00000-0 +55232-3 0 00005
2 67347 43.0004 154.3595 0001374 273.2371 86.8324 15.27594324 05
| Epoch (UTC): | 25 May 2026 07:54:37 |
| Eccentricity: | 0.0001374 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.3595° |
| argument of perigee: | 273.2371° |
| revolutions per day: | 15.27594324 |
| mean anomaly at epoch: | 86.8324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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