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 67473U 26145.34000250 +.00000000 +00000-0 +81124-3 0 00001
2 67473 43.0001 132.4365 0001421 271.9198 88.1491 15.27585765 08
| Epoch (UTC): | 25 May 2026 08:09:36 |
| Eccentricity: | 0.0001421 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.4365° |
| argument of perigee: | 271.9198° |
| revolutions per day: | 15.27585765 |
| mean anomaly at epoch: | 88.1491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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