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 12:07:36 |
| Eccentricity: | 0.0007082 |
| inclination: | 69.9718° |
| perigee height: | 897 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 43.4737° |
| argument of perigee: | 346.4915° |
| revolutions per day: | 13.97693507 |
| mean anomaly at epoch: | 13.6001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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