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 18:42:02 |
| Eccentricity: | 0.0020243 |
| inclination: | 82.5367° |
| perigee height: | 598 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 105.7006° |
| argument of perigee: | 66.6657° |
| revolutions per day: | 14.85530688 |
| mean anomaly at epoch: | 55.4846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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