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 14:07:07 |
| Eccentricity: | 0.0007125 |
| inclination: | 98.2889° |
| perigee height: | 433 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 211.2181° |
| argument of perigee: | 227.5629° |
| revolutions per day: | 15.42742535 |
| mean anomaly at epoch: | 132.5014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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