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 59543U 26145.39332373 +.00000000 +00000-0 -95257-5 0 00004
2 59543 43.0030 270.4740 0001459 276.2503 83.8182 15.27572049 08
| Epoch (UTC): | 25 May 2026 09:26:23 |
| Eccentricity: | 0.0001459 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.4740° |
| argument of perigee: | 276.2503° |
| revolutions per day: | 15.27572049 |
| mean anomaly at epoch: | 83.8182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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