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 23:49:46 |
| Eccentricity: | 0.0015029 |
| inclination: | 74.0510° |
| perigee height: | 753 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 214.4905° |
| argument of perigee: | 109.2529° |
| revolutions per day: | 14.38345517 |
| mean anomaly at epoch: | 251.0253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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