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 00:42:22 |
| Eccentricity: | 0.0368138 |
| inclination: | 100.5143° |
| perigee height: | 933 km |
| apogee height: | 1492 km |
| right ascension of ascending node: | 44.5799° |
| argument of perigee: | 85.1635° |
| revolutions per day: | 13.12848117 |
| mean anomaly at epoch: | 296.4606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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