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 10:02:26 |
| Eccentricity: | 0.0028402 |
| inclination: | 82.9519° |
| perigee height: | 953 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 129.3531° |
| argument of perigee: | 50.0577° |
| revolutions per day: | 13.77191427 |
| mean anomaly at epoch: | 19.7905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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