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 59513U 26145.47577088 +.00000000 +00000-0 +68745-4 0 00004
2 59513 43.0039 204.1006 0001602 289.0658 71.0020 15.27583274 08
| Epoch (UTC): | 25 May 2026 11:25:06 |
| Eccentricity: | 0.0001602 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.1006° |
| argument of perigee: | 289.0658° |
| revolutions per day: | 15.27583274 |
| mean anomaly at epoch: | 71.0020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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