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 58500U 26145.64149059 +.00000000 +00000-0 +15873-3 0 00004
2 58500 46.9822 45.1865 0008951 289.4669 70.5258 14.80558180 04
| Epoch (UTC): | 25 May 2026 15:23:44 |
| Eccentricity: | 0.0008951 |
| inclination: | 46.9822° |
| perigee height: | 621 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 45.1865° |
| argument of perigee: | 289.4669° |
| revolutions per day: | 14.80558180 |
| mean anomaly at epoch: | 70.5258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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