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 45586U 26145.03619858 +.00000000 +00000-0 +48045-3 0 00003
2 45586 53.0400 16.6664 0004434 95.5911 264.5609 15.66803245 08
| Epoch (UTC): | 25 May 2026 00:52:07 |
| Eccentricity: | 0.0004434 |
| inclination: | 53.0400° |
| perigee height: | 365 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 16.6664° |
| argument of perigee: | 95.5911° |
| revolutions per day: | 15.66803245 |
| mean anomaly at epoch: | 264.5609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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