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 04:14:44 |
| Eccentricity: | 0.0007723 |
| inclination: | 51.6333° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 351.7881° |
| argument of perigee: | 8.9804° |
| revolutions per day: | 15.49250518 |
| mean anomaly at epoch: | 351.1321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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