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 18:09:19 |
| Eccentricity: | 0.0020323 |
| inclination: | 82.5369° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 108.5349° |
| argument of perigee: | 75.9400° |
| revolutions per day: | 14.85529074 |
| mean anomaly at epoch: | 90.9769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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