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 07:01:16 |
| Eccentricity: | 0.0029073 |
| inclination: | 81.1939° |
| perigee height: | 844 km |
| apogee height: | 886 km |
| right ascension of ascending node: | 17.8310° |
| argument of perigee: | 64.7688° |
| revolutions per day: | 14.08454822 |
| mean anomaly at epoch: | 295.6490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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