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 06:12:43 |
| Eccentricity: | 0.0033530 |
| inclination: | 82.9183° |
| perigee height: | 950 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 90.7133° |
| argument of perigee: | 65.5587° |
| revolutions per day: | 13.77040235 |
| mean anomaly at epoch: | 353.1864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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