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 58051U 26145.50841992 +.00000000 +00000-0 +60866-4 0 00008
2 58051 43.0029 313.6233 0001333 261.1590 98.9111 15.27580088 07
| Epoch (UTC): | 25 May 2026 12:12:07 |
| Eccentricity: | 0.0001333 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.6233° |
| argument of perigee: | 261.1590° |
| revolutions per day: | 15.27580088 |
| mean anomaly at epoch: | 98.9111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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