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): | 14 January 2026 13:47:26 |
| Eccentricity: | 0.0001314 |
| inclination: | 97.8821° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 200.4057° |
| argument of perigee: | 85.3185° |
| revolutions per day: | 14.82154886 |
| mean anomaly at epoch: | 274.8178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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