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 67055U 26144.97239591 +.00000000 +00000-0 +34872-4 0 00006
2 67055 43.0033 327.4466 0002195 262.4493 97.6109 15.27617370 08
| Epoch (UTC): | 24 May 2026 23:20:15 |
| Eccentricity: | 0.0002195 |
| inclination: | 43.0033° |
| perigee height: | 481 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.4466° |
| argument of perigee: | 262.4493° |
| revolutions per day: | 15.27617370 |
| mean anomaly at epoch: | 97.6109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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