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,
| Epoch (UTC): | 13 January 2026 12:51:36 |
| Eccentricity: | 0.0019715 |
| inclination: | 74.0542° |
| perigee height: | 729 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 168.9286° |
| argument of perigee: | 72.9403° |
| revolutions per day: | 14.44775603 |
| mean anomaly at epoch: | 287.3913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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