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 04:51:06 |
| Eccentricity: | 0.0025355 |
| inclination: | 97.8207° |
| perigee height: | 632 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 351.3597° |
| argument of perigee: | 37.2832° |
| revolutions per day: | 14.73607871 |
| mean anomaly at epoch: | 323.0130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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