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 58160U 26145.38893013 +.00000000 +00000-0 +38329-4 0 00005
2 58160 53.1605 223.2580 0000848 98.1786 261.9312 15.31701292 08
| Epoch (UTC): | 25 May 2026 09:20:03 |
| Eccentricity: | 0.0000848 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 223.2580° |
| argument of perigee: | 98.1786° |
| revolutions per day: | 15.31701292 |
| mean anomaly at epoch: | 261.9312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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