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): | 13 January 2026 11:53:37 |
| Eccentricity: | 0.0140120 |
| inclination: | 89.0706° |
| perigee height: | 788 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 298.1195° |
| argument of perigee: | 4.9894° |
| revolutions per day: | 14.01138516 |
| mean anomaly at epoch: | 355.2643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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