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 58086U 26145.31689036 +.00000000 +00000-0 +14650-2 0 00002
2 58086 43.0024 8.6556 0001226 273.3265 86.7447 15.27619137 09
| Epoch (UTC): | 25 May 2026 07:36:19 |
| Eccentricity: | 0.0001226 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.6556° |
| argument of perigee: | 273.3265° |
| revolutions per day: | 15.27619137 |
| mean anomaly at epoch: | 86.7447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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