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 58078U 26145.61478041 +.00000000 +00000-0 +10825-3 0 00009
2 58078 43.0037 3.1761 0001044 220.2891 139.7883 15.27573311 02
| Epoch (UTC): | 25 May 2026 14:45:17 |
| Eccentricity: | 0.0001044 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.1761° |
| argument of perigee: | 220.2891° |
| revolutions per day: | 15.27573311 |
| mean anomaly at epoch: | 139.7883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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