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 02:08:34 |
| Eccentricity: | 0.0009880 |
| inclination: | 98.5813° |
| perigee height: | 767 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 42.5715° |
| argument of perigee: | 7.6602° |
| revolutions per day: | 14.35382571 |
| mean anomaly at epoch: | 352.4732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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