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 59919U 26137.34851410 +.00000000 +00000-0 +14767-3 0 00009
2 59919 97.5921 154.2007 0041167 4.8198 355.3425 15.19700486 04
| Epoch (UTC): | 17 May 2026 08:21:51 |
| Eccentricity: | 0.0041167 |
| inclination: | 97.5921° |
| perigee height: | 478 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 154.2007° |
| argument of perigee: | 4.8198° |
| revolutions per day: | 15.19700486 |
| mean anomaly at epoch: | 355.3425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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