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): | 11 January 2026 05:53:57 |
| Eccentricity: | 0.0015325 |
| inclination: | 74.0671° |
| perigee height: | 740 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 197.3684° |
| argument of perigee: | 20.4650° |
| revolutions per day: | 14.42304945 |
| mean anomaly at epoch: | 339.7117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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