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 59519U 26145.29531648 +.00000000 +00000-0 -87821-4 0 00009
2 59519 43.0022 234.8180 0001149 270.1686 89.9034 15.27587190 01
| Epoch (UTC): | 25 May 2026 07:05:15 |
| Eccentricity: | 0.0001149 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 234.8180° |
| argument of perigee: | 270.1686° |
| revolutions per day: | 15.27587190 |
| mean anomaly at epoch: | 89.9034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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