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 03:33:52 |
| Eccentricity: | 0.0016328 |
| inclination: | 81.1034° |
| perigee height: | 422 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 67.8068° |
| argument of perigee: | 230.0363° |
| revolutions per day: | 15.44475872 |
| mean anomaly at epoch: | 129.9448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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