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 18586U 26044.89077661 +.00000000 +00000-0 +66736-4 0 00003
2 18586 74.0037 225.6110 0021547 255.1308 104.7459 14.38305579 06
| Epoch (UTC): | 13 February 2026 21:22:43 |
| Eccentricity: | 0.0021547 |
| inclination: | 74.0037° |
| perigee height: | 749 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 225.6110° |
| argument of perigee: | 255.1308° |
| revolutions per day: | 14.38305579 |
| mean anomaly at epoch: | 104.7459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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