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 14:46:25 |
| Eccentricity: | 0.0015519 |
| inclination: | 74.0674° |
| perigee height: | 740 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 189.2801° |
| argument of perigee: | 10.9299° |
| revolutions per day: | 14.42307655 |
| mean anomaly at epoch: | 349.2191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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