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): | 12 January 2026 07:12:43 |
| Eccentricity: | 0.0021118 |
| inclination: | 82.5041° |
| perigee height: | 604 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 320.3462° |
| argument of perigee: | 123.1511° |
| revolutions per day: | 14.83507354 |
| mean anomaly at epoch: | 237.1734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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