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): | 12 January 2026 18:05:57 |
| Eccentricity: | 0.0058616 |
| inclination: | 56.9986° |
| perigee height: | 406 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 126.7297° |
| argument of perigee: | 269.2794° |
| revolutions per day: | 15.40139466 |
| mean anomaly at epoch: | 90.1542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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