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 04:11:35 |
| Eccentricity: | 0.0874754 |
| inclination: | 28.2279° |
| perigee height: | 567 km |
| apogee height: | 1899 km |
| right ascension of ascending node: | 59.0478° |
| argument of perigee: | 128.8195° |
| revolutions per day: | 13.07493990 |
| mean anomaly at epoch: | 239.3762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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