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 14:15:36 |
| Eccentricity: | 0.0019380 |
| inclination: | 82.5113° |
| perigee height: | 599 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 245.3059° |
| argument of perigee: | 56.5830° |
| revolutions per day: | 14.85461630 |
| mean anomaly at epoch: | 303.7237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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