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): | 12 January 2026 01:34:09 |
| Eccentricity: | 0.0020819 |
| inclination: | 74.0247° |
| perigee height: | 736 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 228.5887° |
| argument of perigee: | 201.0992° |
| revolutions per day: | 14.42350598 |
| mean anomaly at epoch: | 158.9307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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