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 58365U 26144.85006593 +.00000000 +00000-0 +22832-4 0 00004
2 58365 43.0026 280.6234 0001807 265.3373 94.7272 15.27572478 03
| Epoch (UTC): | 24 May 2026 20:24:05 |
| Eccentricity: | 0.0001807 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.6234° |
| argument of perigee: | 265.3373° |
| revolutions per day: | 15.27572478 |
| mean anomaly at epoch: | 94.7272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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