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 58451U 26145.50395889 +.00000000 +00000-0 -36645-4 0 00000
2 58451 43.0012 327.6800 0002005 262.0769 97.9855 15.27574338 08
| Epoch (UTC): | 25 May 2026 12:05:42 |
| Eccentricity: | 0.0002005 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.6800° |
| argument of perigee: | 262.0769° |
| revolutions per day: | 15.27574338 |
| mean anomaly at epoch: | 97.9855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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