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 18:53:45 |
| Eccentricity: | 0.0113614 |
| inclination: | 69.9608° |
| perigee height: | 906 km |
| apogee height: | 1073 km |
| right ascension of ascending node: | 181.7788° |
| argument of perigee: | 150.2001° |
| revolutions per day: | 13.72881985 |
| mean anomaly at epoch: | 210.5628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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