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 58161U 26145.59091014 +.00000000 +00000-0 +15530-3 0 00008
2 58161 53.1624 222.3654 0000871 128.0473 232.0607 15.30199595 06
| Epoch (UTC): | 25 May 2026 14:10:54 |
| Eccentricity: | 0.0000871 |
| inclination: | 53.1624° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.3654° |
| argument of perigee: | 128.0473° |
| revolutions per day: | 15.30199595 |
| mean anomaly at epoch: | 232.0607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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