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 26021.32541154 +.00000000 +00000-0 +18521-3 0 00008
2 14059 82.9692 250.4256 0043720 84.7821 275.8325 13.79111312 08
| Epoch (UTC): | 21 January 2026 07:48:35 |
| Eccentricity: | 0.0043720 |
| inclination: | 82.9692° |
| perigee height: | 935 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 250.4256° |
| argument of perigee: | 84.7821° |
| revolutions per day: | 13.79111312 |
| mean anomaly at epoch: | 275.8325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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