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 26040.92618284 +.00000000 +00000-0 +67716-4 0 00004
2 18586 74.0035 232.9310 0021526 262.8909 96.9797 14.38304025 08
| Epoch (UTC): | 09 February 2026 22:13:42 |
| Eccentricity: | 0.0021526 |
| inclination: | 74.0035° |
| perigee height: | 749 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 232.9310° |
| argument of perigee: | 262.8909° |
| revolutions per day: | 14.38304025 |
| mean anomaly at epoch: | 96.9797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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