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 04:18:48 |
| Eccentricity: | 0.1447957 |
| inclination: | 32.8792° |
| perigee height: | 552 km |
| apogee height: | 2898 km |
| right ascension of ascending node: | 307.9019° |
| argument of perigee: | 260.5774° |
| revolutions per day: | 11.90178678 |
| mean anomaly at epoch: | 82.8762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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