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 67179U 26145.56916360 +.00000000 +00000-0 +10951-2 0 00005
2 67179 43.0034 236.4738 0001858 267.0053 93.0586 15.27622435 02
| Epoch (UTC): | 25 May 2026 13:39:35 |
| Eccentricity: | 0.0001858 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.4738° |
| argument of perigee: | 267.0053° |
| revolutions per day: | 15.27622435 |
| mean anomaly at epoch: | 93.0586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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