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 58450U 26144.79370832 +.00000000 +00000-0 +49815-4 0 00002
2 58450 43.0022 331.8046 0001442 261.6080 98.4609 15.27575177 07
| Epoch (UTC): | 24 May 2026 19:02:56 |
| Eccentricity: | 0.0001442 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.8046° |
| argument of perigee: | 261.6080° |
| revolutions per day: | 15.27575177 |
| mean anomaly at epoch: | 98.4609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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