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 67167U 26145.53717979 +.00000000 +00000-0 +58583-3 0 00008
2 67167 42.9993 237.0997 0001564 270.9414 89.1259 15.27614713 06
| Epoch (UTC): | 25 May 2026 12:53:32 |
| Eccentricity: | 0.0001564 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.0997° |
| argument of perigee: | 270.9414° |
| revolutions per day: | 15.27614713 |
| mean anomaly at epoch: | 89.1259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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