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 17:02:09 |
| Eccentricity: | 0.0028136 |
| inclination: | 81.2463° |
| perigee height: | 842 km |
| apogee height: | 883 km |
| right ascension of ascending node: | 116.5394° |
| argument of perigee: | 53.5977° |
| revolutions per day: | 14.09096262 |
| mean anomaly at epoch: | 306.7782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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