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 14:49:30 |
| Eccentricity: | 0.0003915 |
| inclination: | 97.6160° |
| perigee height: | 548 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 33.4958° |
| argument of perigee: | 325.6654° |
| revolutions per day: | 15.05291326 |
| mean anomaly at epoch: | 34.4319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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