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): | 14 January 2026 13:12:18 |
| Eccentricity: | 0.0002398 |
| inclination: | 97.9702° |
| perigee height: | 688 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 70.0230° |
| argument of perigee: | 25.1909° |
| revolutions per day: | 14.60943795 |
| mean anomaly at epoch: | 83.1792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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