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 59333U 26145.42430389 +.00000000 +00000-0 +81660-4 0 00002
2 59333 43.0001 125.0456 0001645 272.0928 87.9735 15.27583162 01
| Epoch (UTC): | 25 May 2026 10:10:59 |
| Eccentricity: | 0.0001645 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.0456° |
| argument of perigee: | 272.0928° |
| revolutions per day: | 15.27583162 |
| mean anomaly at epoch: | 87.9735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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