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 14:06:14 |
| Eccentricity: | 0.0002609 |
| inclination: | 87.3370° |
| perigee height: | 423 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 112.7929° |
| argument of perigee: | 96.5118° |
| revolutions per day: | 15.47356530 |
| mean anomaly at epoch: | 263.6438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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