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 67906U 26145.35685860 +.00000000 +00000-0 +51883-3 0 00008
2 67906 43.0008 172.6164 0001654 276.4962 83.5701 15.27591730 08
| Epoch (UTC): | 25 May 2026 08:33:52 |
| Eccentricity: | 0.0001654 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 172.6164° |
| argument of perigee: | 276.4962° |
| revolutions per day: | 15.27591730 |
| mean anomaly at epoch: | 83.5701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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