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 13:25:31 |
| Eccentricity: | 0.0076594 |
| inclination: | 65.0773° |
| perigee height: | 635 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 129.9280° |
| argument of perigee: | 309.5346° |
| revolutions per day: | 14.61305389 |
| mean anomaly at epoch: | 49.9001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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