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): | 16 January 2026 06:34:47 |
| Eccentricity: | 0.0019138 |
| inclination: | 97.8663° |
| perigee height: | 543 km |
| apogee height: | 569 km |
| right ascension of ascending node: | 33.6404° |
| argument of perigee: | 189.5337° |
| revolutions per day: | 15.03504214 |
| mean anomaly at epoch: | 170.5527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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