Voyager LECP Data Analysis Handbook
Data File Descriptions
Super Average Tape Record Description
Trajectory Footnotes
THE FOLLOWING ITEMS,
54-65 AND 70-72, ARE TRAJECTORY DATA WHICH HAVE
DIFFERENT ITEMS FOR CRUISE, JUPITER, SATURN, URANUS,
AND NEPTUNE. IN GENERAL, THE COORDINATE FOR
SATELLITES IS PLANET CENTERED, PLANET MEAN ORBIT,
AND PRIME MERIDIAN IN SUN DIRECTION. HOWEVER, THE
COORDINATE FOR SUN IS PLANET CENTERED, EARTH MEAN
ECLIPTIC AND EQUINOX OF 1950.0 (ECL50). 1 AU (ASTRONOMICAL UNIT = 1.496E08 KM) |
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MISSION PHASE |
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Item # | Name | Type | Cruise (EME1950) | Jupiter (EME50) |
Saturn | Uranus | Neptune | Coord | Units |
---|---|---|---|---|---|---|---|---|---|
SUNX |
I*2 |
SUN |
SUN |
SUN |
SUN |
SUN |
X |
0.01 AU |
|
SUNY |
I*2 |
SUN |
SUN |
SUN |
SUN |
SUN |
Y | 0.01 AU | |
SUNZ |
I*2 |
SUN, |
SUN |
SUN |
SUN |
SUN, |
Z | 0.01 AU | |
SAT1X |
I*2 |
EARTH |
IO |
TITAN |
MIRANDA |
TRITON |
X | 0.01 RP | |
SAT1Y |
I*2 |
EARTH |
IO, |
TITAN |
MIRANDA | TRITON | Y | 0.01 RP | |
SAT1Z |
I*2 |
EARTH |
IO |
TITAN |
MIRANDA | TRITON | Z | 0.01 RP | |
SAT2X |
I*2 |
JUPITER |
EUROPA |
RHEA |
ARIEL |
1989N1 |
X | 0.01 RP | |
SAT2Y |
I*2 |
JUPITER |
EUROPA |
RHEA |
ARIEL | 1989N1 | Y | 0.01 RP | |
SAT2Z |
I*2 |
JUPITER |
EUROPA |
RHEA |
ARIEL | 1989N1 | Z | 0.01 RP | |
SAT3X |
I*2 |
SATURN |
GANYMEDE |
DIONE |
UMBRIEL |
1989N2 |
X | 0.01 RP | |
SAT3Y |
I*2 |
SATURN |
GANYMEDE |
DIONE |
UMBRIEL | 1989N2 | Y | 0.01 RP | |
SAT3Z |
I*2 |
SATURN |
GANYMEDE |
DIONE |
UMBRIEL | 1989N2 | Z | 0.01 RP | |
SAT4X |
I*2 |
CALLISTO |
MIMAS |
TITANIA |
1989N3 |
X | 0.01 RP | ||
SAT4Y |
I*2 |
CALLISTO |
MIMAS |
TITANIA | 1989N3 | Y | 0.01 RP | ||
SAT4Z |
I*2 |
CALLISTO |
MIMAS |
TITANIA | 1989N3 | Z | 0.01 RP |
Additional details on Jupiter trajectory data:
Item | Name | Type | ||
54 | SUNX | SEDR, -(55)(1.496E06) | I*2 | X coordinate of Sun, units of 0.01 AU |
55 | SUNY | SEDR, -(56)(1.496E06) | I*2 | Y coordinate of Sun, units of 0.01 AU |
56 | SUNZ | SEDR, -(57)(1.496E06) | I*2 | Z coordinate of Sun, units of 0.01 AU |
57 | SAT1X | IO, SEDR, (97)/(713) | I*2 | X coordinate of Satellite 1, units of 0.01 Rp |
58 | SAT1Y | IO, SEDR, (98)/(713) | I*2 | Y coordinate of Satellite 1, units of 0.01 Rp |
59 | SAT1Z | IO, SEDR, (99)/(713) | I*2 | Z coordinate of Satellite 1, units of 0.01 Rp |
60 | SAT2X | EUROPA, SEDR, (103)/(713) | I*2 | X coordinate of Satellite 2, units of 0.01 Rp |
61 | SAT2Y | EUROPA, SEDR, (104)/(713) | I*2 | Y coordinate of Satellite 2, units of 0.01 Rp |
62 | SAT2Z | EUROPA, SEDR, (105)/(713) | I*2 | Z coordinate of Satellite 2 units of 0.01 Rp |
63 | SAT3X | GANYMEDE, SEDR, (109)/(713) | I*2 | X coordinate of Satellite 3, units of 0.01 Rp |
64 | SAT3Y | GANYMEDE, SEDR, (110)/(713) | I*2 | Y coordinate of Satellite 3, units of 0.01 Rp |
65 | SAT3Z | GANYMEDE, SEDR, (111)/(713) | I*2 | Z coordinate of Satellite 13 units of 0.01 Rp |
66 | NAMEIN | A*2 | 1st and 2nd characters of input filename | |
67 | NAMEIN | A*2 | 3rd and 4th characters of input filename | |
68 | NAMEIN | A*2 | 5th and 6th characters of input filename | |
69 | NAMEIN | A*2 | 7th and 8th characters of input filename | |
70 | SAT4X | CALLISTO, SEDR,(115)/(713) | I*2 | X coordinate of Satellite 4, units of 0.01 Rp |
71 | SAT4Y | CALLISTO, SEDR,(116)/(713) | I*2 | Y coordinate of Satellite 4, units of 0.01 Rp |
72 | SAT4Z | CALLISTO, SEDR,(117)/(713) | I*2 | Z coordinate of Satellite 4, units of 0.01 Rp |
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LECP Data Analysis Handbook Table of Contents.
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Technologies Home Page.
Updated 8/9/19, Cameron Crane
VOYAGER 1 ELAPSED TIME
*Since official launch
September 5, 1977, 12:56:00:00 UTC
VOYAGER 2 ELAPSED TIME
*Since official launch
August 20, 1977, 14:29:00:00 UTC
QUICK FACTS
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.