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 59737U 26145.35171360 +.00000000 +00000-0 +50151-4 0 00004
2 59737 43.0032 110.6351 0001041 281.6367 78.4368 15.27590559 05
| Epoch (UTC): | 25 May 2026 08:26:28 |
| Eccentricity: | 0.0001041 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.6351° |
| argument of perigee: | 281.6367° |
| revolutions per day: | 15.27590559 |
| mean anomaly at epoch: | 78.4368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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