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 67175U 26145.25378566 +.00000000 +00000-0 +59406-3 0 00006
2 67175 43.0020 238.4067 0001070 273.3651 86.7078 15.27615897 09
| Epoch (UTC): | 25 May 2026 06:05:27 |
| Eccentricity: | 0.0001070 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 238.4067° |
| argument of perigee: | 273.3651° |
| revolutions per day: | 15.27615897 |
| mean anomaly at epoch: | 86.7078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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