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 18:51:21 |
| Eccentricity: | 0.0256402 |
| inclination: | 66.6935° |
| perigee height: | 589 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 45.9398° |
| argument of perigee: | 271.1516° |
| revolutions per day: | 14.35825630 |
| mean anomaly at epoch: | 86.0224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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