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 59076U 26145.30885890 +.00000000 +00000-0 -10061-3 0 00001
2 59076 43.0013 237.6435 0000623 277.5610 82.5170 15.27565461 04
| Epoch (UTC): | 25 May 2026 07:24:45 |
| Eccentricity: | 0.0000623 |
| inclination: | 43.0013° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.6435° |
| argument of perigee: | 277.5610° |
| revolutions per day: | 15.27565461 |
| mean anomaly at epoch: | 82.5170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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