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 12:42:23 |
| Eccentricity: | 0.0026305 |
| inclination: | 74.0310° |
| perigee height: | 540 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 64.3238° |
| argument of perigee: | 261.3999° |
| revolutions per day: | 15.02792307 |
| mean anomaly at epoch: | 98.4209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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