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 14:15:18 |
| Eccentricity: | 0.0063428 |
| inclination: | 61.9946° |
| perigee height: | 522 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 41.6956° |
| argument of perigee: | 100.5457° |
| revolutions per day: | 15.00243200 |
| mean anomaly at epoch: | 260.2786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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