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 04:10:33 |
| Eccentricity: | 0.0061203 |
| inclination: | 81.2933° |
| perigee height: | 823 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 278.2866° |
| argument of perigee: | 90.3541° |
| revolutions per day: | 14.07733927 |
| mean anomaly at epoch: | 270.4642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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