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 58512U 26145.03863427 +.00000000 +00000-0 +46769-4 0 00001
2 58512 43.0018 32.6187 0000516 269.3370 90.7423 15.27585285 01
| Epoch (UTC): | 25 May 2026 00:55:38 |
| Eccentricity: | 0.0000516 |
| inclination: | 43.0018° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 32.6187° |
| argument of perigee: | 269.3370° |
| revolutions per day: | 15.27585285 |
| mean anomaly at epoch: | 90.7423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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