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 67310U 26145.56739162 +.00000000 +00000-0 +74275-3 0 00005
2 67310 43.0009 251.3463 0000912 262.4787 97.5961 15.27595333 07
| Epoch (UTC): | 25 May 2026 13:37:02 |
| Eccentricity: | 0.0000912 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.3463° |
| argument of perigee: | 262.4787° |
| revolutions per day: | 15.27595333 |
| mean anomaly at epoch: | 97.5961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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