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 13:59:20 |
| Eccentricity: | 0.0059479 |
| inclination: | 97.2411° |
| perigee height: | 895 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 327.0720° |
| argument of perigee: | 257.4619° |
| revolutions per day: | 13.87103751 |
| mean anomaly at epoch: | 101.9886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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