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 07:39:58 |
| Eccentricity: | 0.0012613 |
| inclination: | 71.0038° |
| perigee height: | 831 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 4.4287° |
| argument of perigee: | 323.7035° |
| revolutions per day: | 14.15724319 |
| mean anomaly at epoch: | 135.6942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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