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 05:31:58 |
| Eccentricity: | 0.0006855 |
| inclination: | 71.0550° |
| perigee height: | 840 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 293.2192° |
| argument of perigee: | 123.0079° |
| revolutions per day: | 14.14362852 |
| mean anomaly at epoch: | 237.1703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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