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): | 14 January 2026 12:52:09 |
| Eccentricity: | 0.1088005 |
| inclination: | 63.3058° |
| perigee height: | 1196 km |
| apogee height: | 3046 km |
| right ascension of ascending node: | 103.6280° |
| argument of perigee: | 67.7341° |
| revolutions per day: | 11.07972180 |
| mean anomaly at epoch: | 16.5364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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