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 67122U 26145.19201163 +.00000000 +00000-0 +49938-3 0 00008
2 67122 43.0042 97.1717 0001856 259.1001 100.9642 15.27591036 04
| Epoch (UTC): | 25 May 2026 04:36:29 |
| Eccentricity: | 0.0001856 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 97.1717° |
| argument of perigee: | 259.1001° |
| revolutions per day: | 15.27591036 |
| mean anomaly at epoch: | 100.9642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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