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 26038.00490093 +.00000000 +00000-0 +71990-4 0 00005
2 18586 74.0035 238.3243 0021545 268.6419 91.2266 14.38302913 07
| Epoch (UTC): | 07 February 2026 00:07:03 |
| Eccentricity: | 0.0021545 |
| inclination: | 74.0035° |
| perigee height: | 749 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 238.3243° |
| argument of perigee: | 268.6419° |
| revolutions per day: | 14.38302913 |
| mean anomaly at epoch: | 91.2266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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