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 01:54:30 |
| Eccentricity: | 0.0013756 |
| inclination: | 82.5289° |
| perigee height: | 942 km |
| apogee height: | 962 km |
| right ascension of ascending node: | 52.7524° |
| argument of perigee: | 271.5546° |
| revolutions per day: | 13.83387940 |
| mean anomaly at epoch: | 107.4520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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