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 14450U 26106.86547161 +.00000000 +00000-0 +28534-4 0 00006
2 14450 82.9291 317.2089 0042972 171.0400 199.7171 13.76535149 03
| Epoch (UTC): | 16 April 2026 20:46:16 |
| Eccentricity: | 0.0042972 |
| inclination: | 82.9291° |
| perigee height: | 945 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 317.2089° |
| argument of perigee: | 171.0400° |
| revolutions per day: | 13.76535149 |
| mean anomaly at epoch: | 199.7171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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