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 20:20:29 |
| Eccentricity: | 0.0003331 |
| inclination: | 70.9991° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 183.9585° |
| argument of perigee: | 339.8073° |
| revolutions per day: | 14.15005511 |
| mean anomaly at epoch: | 20.2917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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