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 46758U 26145.58335647 +.00000000 +00000-0 +81384-3 0 00009
2 46758 53.0378 261.0559 0007473 296.9820 134.0499 15.87132718 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0007473 |
| inclination: | 53.0378° |
| perigee height: | 305 km |
| apogee height: | 315 km |
| right ascension of ascending node: | 261.0559° |
| argument of perigee: | 296.9820° |
| revolutions per day: | 15.87132718 |
| mean anomaly at epoch: | 134.0499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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