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 58361U 26145.42054902 +.00000000 +00000-0 +72031-4 0 00007
2 58361 43.0045 277.1692 0001573 261.3291 98.7383 15.27579568 08
| Epoch (UTC): | 25 May 2026 10:05:35 |
| Eccentricity: | 0.0001573 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.1692° |
| argument of perigee: | 261.3291° |
| revolutions per day: | 15.27579568 |
| mean anomaly at epoch: | 98.7383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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