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): | 13 January 2026 12:41:14 |
| Eccentricity: | 0.0001960 |
| inclination: | 28.4674° |
| perigee height: | 479 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 56.0330° |
| argument of perigee: | 208.9714° |
| revolutions per day: | 15.28524210 |
| mean anomaly at epoch: | 151.0772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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