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 18583U 26140.30525742 +.00000000 +00000-0 +00000-0 0 00009
2 18583 12.0807 338.5154 0026320 280.5162 74.9839 0.98388649 06
| Epoch (UTC): | 20 May 2026 07:19:34 |
| Eccentricity: | 0.0026320 |
| inclination: | 12.0807° |
| perigee height: | 36211 km |
| apogee height: | 36435 km |
| right ascension of ascending node: | 338.5154° |
| argument of perigee: | 280.5162° |
| revolutions per day: | 0.98388649 |
| mean anomaly at epoch: | 74.9839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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