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): | 15 January 2026 17:56:36 |
| Eccentricity: | 0.0017078 |
| inclination: | 70.9779° |
| perigee height: | 834 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 142.9334° |
| argument of perigee: | 116.2911° |
| revolutions per day: | 14.13747911 |
| mean anomaly at epoch: | 243.9968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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