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 67046U 26145.49679338 +.00000000 +00000-0 +31264-3 0 00002
2 67046 43.0020 324.5020 0001819 265.2245 94.8399 15.27585516 02
| Epoch (UTC): | 25 May 2026 11:55:22 |
| Eccentricity: | 0.0001819 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.5020° |
| argument of perigee: | 265.2245° |
| revolutions per day: | 15.27585516 |
| mean anomaly at epoch: | 94.8399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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