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 15:26:28 |
| Eccentricity: | 0.0037631 |
| inclination: | 82.9572° |
| perigee height: | 945 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 261.1661° |
| argument of perigee: | 103.9675° |
| revolutions per day: | 13.77490037 |
| mean anomaly at epoch: | 256.5671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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