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 15:34:50 |
| Eccentricity: | 0.0024590 |
| inclination: | 82.9416° |
| perigee height: | 960 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 55.1581° |
| argument of perigee: | 162.9533° |
| revolutions per day: | 13.75985698 |
| mean anomaly at epoch: | 313.6667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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