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 58592U 26145.55520581 +.00000000 +00000-0 +15955-2 0 00008
2 58592 42.9964 94.9767 0009822 170.9978 189.1053 15.31797212 04
| Epoch (UTC): | 25 May 2026 13:19:29 |
| Eccentricity: | 0.0009822 |
| inclination: | 42.9964° |
| perigee height: | 464 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 94.9767° |
| argument of perigee: | 170.9978° |
| revolutions per day: | 15.31797212 |
| mean anomaly at epoch: | 189.1053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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