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 59152U 26145.60348902 +.00000000 +00000-0 +38544-4 0 00003
2 59152 43.0035 341.9604 0001405 268.5132 91.5559 15.27572559 05
| Epoch (UTC): | 25 May 2026 14:29:01 |
| Eccentricity: | 0.0001405 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.9604° |
| argument of perigee: | 268.5132° |
| revolutions per day: | 15.27572559 |
| mean anomaly at epoch: | 91.5559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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