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 19:30:12 |
| Eccentricity: | 0.0034622 |
| inclination: | 35.0015° |
| perigee height: | 613 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 273.1701° |
| argument of perigee: | 260.3414° |
| revolutions per day: | 14.77505616 |
| mean anomaly at epoch: | 99.3374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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