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): | 13 January 2026 15:27:29 |
| Eccentricity: | 0.0685460 |
| inclination: | 63.3886° |
| perigee height: | 485 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 104.0616° |
| argument of perigee: | 2.2677° |
| revolutions per day: | 13.72757386 |
| mean anomaly at epoch: | 358.1207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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