VOYAGER
Voyager LECP Data Analysis Handbook
Data File Descriptions
Supplementary EDR
Figure E-1.
Earth Mean Ecliptic and Equinox of 1950.0 (ECL50), Jupiter Encounter State Vectors
Nomenclature --> S refers to State Vector (position and velocity components) with the subscripts AB, where A is the reference or "from" body and B is the "to" body. The following body definitions are used: S - Sun; P - S/C or Probe; E - Earth; 5 - Jupiter; I - Io; U - Europa; G - Ganymede; C - Callisto.
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Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
September 5, 1977, 12:56:00:00 UTC
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
--:--:--:--
Days: Hours:
Minutes: Seconds
*Since official launch
August 20, 1977, 14:29:00:00 UTC
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
Manufacturer:
Voyagers 1 and 2 were built in the Jet Propulsion
Laboratory in Southern California.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.
Mission Duration: 40+ years have elapsed for both Voyager 1 and Voyager 2 (both are ongoing).
Destination: Their original destinations were Saturn and Jupiter. Their current destination is interstellar space.