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): | 11 January 2026 06:55:19 |
| Eccentricity: | 0.0031310 |
| inclination: | 98.8164° |
| perigee height: | 747 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 25.7323° |
| argument of perigee: | 228.0473° |
| revolutions per day: | 14.36752741 |
| mean anomaly at epoch: | 131.8043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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