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,
1 14059U 26020.74499935 +.00000000 +00000-0 +18872-3 0 00001
2 14059 82.9692 250.8569 0043719 86.3617 274.2540 13.79111130 08
| Epoch (UTC): | 20 January 2026 17:52:47 |
| Eccentricity: | 0.0043719 |
| inclination: | 82.9692° |
| perigee height: | 935 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 250.8569° |
| argument of perigee: | 86.3617° |
| revolutions per day: | 13.79111130 |
| mean anomaly at epoch: | 274.2540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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