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): | 15 January 2026 19:57:54 |
| Eccentricity: | 0.0016106 |
| inclination: | 71.0084° |
| perigee height: | 822 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 144.2709° |
| argument of perigee: | 283.5013° |
| revolutions per day: | 14.17632802 |
| mean anomaly at epoch: | 191.1736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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