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): | 15 January 2026 02:02:35 |
| Eccentricity: | 0.0036996 |
| inclination: | 67.9873° |
| perigee height: | 514 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 191.1853° |
| argument of perigee: | 103.1782° |
| revolutions per day: | 15.09049816 |
| mean anomaly at epoch: | 257.3499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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