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 58119U 26145.48363789 +.00000000 +00000-0 +82368-4 0 00004
2 58119 43.0072 58.6308 0001788 269.1422 90.9225 15.27581882 06
| Epoch (UTC): | 25 May 2026 11:36:26 |
| Eccentricity: | 0.0001788 |
| inclination: | 43.0072° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.6308° |
| argument of perigee: | 269.1422° |
| revolutions per day: | 15.27581882 |
| mean anomaly at epoch: | 90.9225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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