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 32711U 26145.20262984 +.00000000 +00000-0 +00000-0 0 00008
2 32711 54.4938 150.8428 0210720 247.5440 110.2375 2.00571835 05
| Epoch (UTC): | 25 May 2026 04:51:47 |
| Eccentricity: | 0.0210720 |
| inclination: | 54.4938° |
| perigee height: | 19622 km |
| apogee height: | 20741 km |
| right ascension of ascending node: | 150.8428° |
| argument of perigee: | 247.5440° |
| revolutions per day: | 2.00571835 |
| mean anomaly at epoch: | 110.2375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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