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 58058U 26145.47116443 +.00000000 +00000-0 +73629-4 0 00008
2 58058 43.0030 313.3450 0001646 264.8664 95.2000 15.27575544 01
| Epoch (UTC): | 25 May 2026 11:18:28 |
| Eccentricity: | 0.0001646 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.3450° |
| argument of perigee: | 264.8664° |
| revolutions per day: | 15.27575544 |
| mean anomaly at epoch: | 95.2000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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