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 22:58:03 |
| Eccentricity: | 0.5382758 |
| inclination: | 49.3493° |
| perigee height: | 307 km |
| apogee height: | 15895 km |
| right ascension of ascending node: | 215.6417° |
| argument of perigee: | 86.6822° |
| revolutions per day: | 4.98300076 |
| mean anomaly at epoch: | 330.5463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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