This interface provides access to hourly resolution "impact
parameters" for pairs of Moon and IMP 8, Wind, ACE Geotail and Earth.
These are the distances by which a plasma element moving
radially away from the sun with a speed of 390 km/s,
observed at an upstream spacecraft would miss intercepting
a downstream spacecraft (or Earth), allowing for the
30 km/s motion of the Earth and its nearby spacecraft
about the sun. Dij, the impact parameter for the i-j pair of
bodies, is given by SQRT {[Yi-Yj + (Xi-Xj)/13]**2 + (Zi-Zj)**2}.
For a schematic figure and further description click
HERE.
IMP 1974-01-01 - 2006-12-31 Geotail 1995-08-09 - 2023-01-01 ACE 1998-01-01 - 2024-09-30 Moon 1969-01-01 - 2024-09-30 WIND 1995-01-01 - 2024-09-30Please enter your selections and then click on the Submit button.
If you have any questions/comments about the OMNWeb Plus, contact
Dr. Natalia Papitashvili,Mail Code 672,
NASA/Goddard Space Flight Center, Greenbelt, MD 20771 |