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 58645U 26145.57476008 +.00000000 +00000-0 +19219-3 0 00001
2 58645 97.3461 167.4903 0010845 86.6125 273.6355 15.26720317 01
| Epoch (UTC): | 25 May 2026 13:47:39 |
| Eccentricity: | 0.0010845 |
| inclination: | 97.3461° |
| perigee height: | 478 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 167.4903° |
| argument of perigee: | 86.6125° |
| revolutions per day: | 15.26720317 |
| mean anomaly at epoch: | 273.6355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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