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 56186U 26145.60332416 +.00000000 +00000-0 +25509-3 0 00006
2 56186 97.3007 54.4482 0006165 130.1647 230.0146 15.52214878 00
| Epoch (UTC): | 25 May 2026 14:28:47 |
| Eccentricity: | 0.0006165 |
| inclination: | 97.3007° |
| perigee height: | 406 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 54.4482° |
| argument of perigee: | 130.1647° |
| revolutions per day: | 15.52214878 |
| mean anomaly at epoch: | 230.0146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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