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 11:48:15 |
| Eccentricity: | 0.0144382 |
| inclination: | 97.4016° |
| perigee height: | 609 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 26.2312° |
| argument of perigee: | 183.6075° |
| revolutions per day: | 14.54387089 |
| mean anomaly at epoch: | 176.4097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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