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 43187U 26145.24766605 +.00000000 +00000-0 +22477-3 0 00005
2 43187 97.5385 50.1690 0010782 92.8787 267.3680 15.16387299 05
| Epoch (UTC): | 25 May 2026 05:56:38 |
| Eccentricity: | 0.0010782 |
| inclination: | 97.5385° |
| perigee height: | 509 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 50.1690° |
| argument of perigee: | 92.8787° |
| revolutions per day: | 15.16387299 |
| mean anomaly at epoch: | 267.3680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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