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 67172U 26145.59743902 +.00000000 +00000-0 +74317-3 0 00008
2 67172 43.0000 236.6895 0001436 264.0602 96.0086 15.27598647 08
| Epoch (UTC): | 25 May 2026 14:20:18 |
| Eccentricity: | 0.0001436 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.6895° |
| argument of perigee: | 264.0602° |
| revolutions per day: | 15.27598647 |
| mean anomaly at epoch: | 96.0086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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