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 26041.89994306 +.00000000 +00000-0 +68149-4 0 00004
2 18586 74.0036 231.1332 0021521 260.9794 98.8924 14.38304413 04
| Epoch (UTC): | 10 February 2026 21:35:55 |
| Eccentricity: | 0.0021521 |
| inclination: | 74.0036° |
| perigee height: | 749 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 231.1332° |
| argument of perigee: | 260.9794° |
| revolutions per day: | 14.38304413 |
| mean anomaly at epoch: | 98.8924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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