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 59324U 26145.38206718 +.00000000 +00000-0 +61738-4 0 00008
2 59324 43.0030 114.3450 0001296 269.4885 90.5818 15.27581646 09
| Epoch (UTC): | 25 May 2026 09:10:10 |
| Eccentricity: | 0.0001296 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.3450° |
| argument of perigee: | 269.4885° |
| revolutions per day: | 15.27581646 |
| mean anomaly at epoch: | 90.5818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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