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 38667U 26081.39127406 +.00000000 +00000-0 +65108-4 0 00006
2 38667 74.0493 124.5727 0021712 315.7440 44.1976 14.36961256 08
| Epoch (UTC): | 22 March 2026 09:23:26 |
| Eccentricity: | 0.0021712 |
| inclination: | 74.0493° |
| perigee height: | 753 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 124.5727° |
| argument of perigee: | 315.7440° |
| revolutions per day: | 14.36961256 |
| mean anomaly at epoch: | 44.1976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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