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): | 14 January 2026 12:47:42 |
| Eccentricity: | 0.0093090 |
| inclination: | 81.2492° |
| perigee height: | 790 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 48.2492° |
| argument of perigee: | 312.6409° |
| revolutions per day: | 14.10640667 |
| mean anomaly at epoch: | 46.6940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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