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 59847U 26145.46479444 +.00000000 +00000-0 -37076-5 0 00005
2 59847 43.0016 201.1982 0000895 280.3622 79.7129 15.27573735 07
| Epoch (UTC): | 25 May 2026 11:09:18 |
| Eccentricity: | 0.0000895 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 201.1982° |
| argument of perigee: | 280.3622° |
| revolutions per day: | 15.27573735 |
| mean anomaly at epoch: | 79.7129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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