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 10:33:15 |
| Eccentricity: | 0.0005800 |
| inclination: | 69.9335° |
| perigee height: | 525 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 17.3158° |
| argument of perigee: | 230.4307° |
| revolutions per day: | 15.12371535 |
| mean anomaly at epoch: | 129.6347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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