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): | 12 January 2026 17:55:45 |
| Eccentricity: | 0.0869016 |
| inclination: | 82.4882° |
| perigee height: | 399 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 275.6922° |
| argument of perigee: | 248.1529° |
| revolutions per day: | 13.57848336 |
| mean anomaly at epoch: | 102.5063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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