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 58114U 26145.45427654 +.00000000 +00000-0 -25803-4 0 00000
2 58114 53.1599 169.0327 0001349 76.2980 283.8170 15.30195840 05
| Epoch (UTC): | 25 May 2026 10:54:09 |
| Eccentricity: | 0.0001349 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.0327° |
| argument of perigee: | 76.2980° |
| revolutions per day: | 15.30195840 |
| mean anomaly at epoch: | 283.8170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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