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 58675U 26145.34718597 +.00000000 +00000-0 +21972-4 0 00001
2 58675 43.0034 11.8986 0000705 278.2367 81.8405 15.27577602 05
| Epoch (UTC): | 25 May 2026 08:19:56 |
| Eccentricity: | 0.0000705 |
| inclination: | 43.0034° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 11.8986° |
| argument of perigee: | 278.2367° |
| revolutions per day: | 15.27577602 |
| mean anomaly at epoch: | 81.8405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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