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 67171U 26145.59999086 +.00000000 +00000-0 +84453-3 0 00005
2 67171 42.9994 236.7101 0001947 276.8968 83.1662 15.27610953 03
| Epoch (UTC): | 25 May 2026 14:23:59 |
| Eccentricity: | 0.0001947 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.7101° |
| argument of perigee: | 276.8968° |
| revolutions per day: | 15.27610953 |
| mean anomaly at epoch: | 83.1662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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