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 58181U 26145.49895550 +.00000000 +00000-0 +38612-4 0 00003
2 58181 43.0032 69.4849 0000737 288.0706 72.0065 15.27577990 07
| Epoch (UTC): | 25 May 2026 11:58:29 |
| Eccentricity: | 0.0000737 |
| inclination: | 43.0032° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.4849° |
| argument of perigee: | 288.0706° |
| revolutions per day: | 15.27577990 |
| mean anomaly at epoch: | 72.0065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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