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 13:59:58 |
| Eccentricity: | 0.0011356 |
| inclination: | 41.4651° |
| perigee height: | 378 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 171.0226° |
| argument of perigee: | 290.8087° |
| revolutions per day: | 15.60531969 |
| mean anomaly at epoch: | 69.1535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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