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 58519U 26144.95782257 +.00000000 +00000-0 -19882-5 0 00007
2 58519 43.0034 32.8187 0001240 250.1967 109.8751 15.27576444 06
| Epoch (UTC): | 24 May 2026 22:59:15 |
| Eccentricity: | 0.0001240 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 32.8187° |
| argument of perigee: | 250.1967° |
| revolutions per day: | 15.27576444 |
| mean anomaly at epoch: | 109.8751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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