urn:nasa:pds:voyager1_rss_jupiter_raw:geometry:vg1_traj_ing 1.0 1.16.0.0 Product_Observational Simpson, R. A. 2021 Trajectory data for the Voyager 1 Jupiter ingress radio occultation, recovered from NSSDCA Merged Occultation Data. These are probably from a Voyager 1 trajectory reconstructed within 18 months of the encounter. There is almost no documentation accompanying the file in NSSDCA. 2021-11-26 1.0 Initial version of data recovered from NSSDCA and converted to a pair of PDS4 tables. The data have been reformatted into physical records that are commensurate with the original logical records. Records are delimited by carriage-return line-feed pairs. A new PDS4 label has been generated. 1979-03-05T14:05:00Z 1979-03-05T16:40:00Z Calibration Derived Trajectory data for the Voyager 1 Jupiter ingress radio occultation. =Voyager Mission urn:nasa:pds:context:investigation:mission.voyager data_to_investigation Voyager Navigation Literature Search Reconstructed spacecraft trajectory during Jupiter encounter using radio tracking and other data. Jupiter Planet urn:nasa:pds:context:target:planet.jupiter data_to_target PSPA-00347:dr005500_f00001.phys.1 data_to_derived_source_product NSSDCA The value of external_source_product_identifier is constructed from the NSSDCA identifier, an ASCII colon, and the file name. vg1_traj_ing.tab 2021-09-08T16:59:00 278024 05e0255dd308ab66921a2e8c47df806c This file was copied from the external source product with minor reformatting to create two Table_Character data objects. The first contains one identifying header record; the second contains many data records. Each record is delimited by a Carriage-Return Line-Feed pair. 0 1 This Table has one header record with ten fixed-width fields followed by one Carriage-Return Line-Feed record delimiter. Carriage-Return Line-Feed 10 0 242 Number of Data Records 1 1 ASCII_Integer 10 %10d The number of data records in the file. Spacecraft ID 2 11 ASCII_Integer 10 %10d The spacecraft identifying number. Values may be 31 = Voyager 1 32 = Voyager 2 Unused Field 1 3 21 ASCII_Integer 10 %10d This field is not used. Value set to '0'. Occultation Sense 4 31 ASCII_Integer 10 %10d The sense of the occultation, given as an integer: 1 = ingress 2 = egress Unused Field 2 5 81 ASCII_Real 20 %20.16f Unused field; value set to .0000000000000000 Ephemeris Time Minus Civil Universal Time 6 105 ASCII_Real 24 %24.16e second Ephemeris Time minus Civil Universal Time. One-Way Light Time 7 129 ASCII_Real 24 %24.16e second One-way light time (approximate). Sun Position (x) 8 161 ASCII_Real 24 %24.16e km x-coordinate of the Sun's position in EME 1950 Jupiter-centered coordinates. Sun Position (y) 9 185 ASCII_Real 24 %24.16e km y-coordinate of the Sun's position in EME 1950 Jupiter-centered coordinates. Sun Position (z) 10 209 ASCII_Real 24 %24.16e km z-coordinate of the Sun's position in EME 1950 Jupiter-centered coordinates. 242 691 This Table_Character has many records with trajectory data. Carriage-Return Line-Feed 18 0 402 ET seconds 1 1 ASCII_Real 26 %26.14e ˚Ephemeris Time in seconds from 1950.0 ET Year 2 31 ASCII_Real 7 %7.1f Ephemeris Time: two-digit year (for example, 79.0 is 1979) from field 1 ET Day 3 38 ASCII_Real 7 %7.1f day Ephemeris Time: day of year (for example, 64.0 is March 5 in 1979) from field 1 ET Hour 4 45 ASCII_Real 7 %7.1f hour Ephemeris Time: hour of day from field 1 ET Minute 5 52 ASCII_Real 7 %7.1f minute Ephemeris Time: minute of hour from field 1 ET Second 6 59 ASCII_Real 14 %14.8f second Ephemeris Time: seconds of minute from field 1 Spacecraft Position (x) 7 81 ASCII_Real 24 %24.16e km x-component of the spacecraft position in EME 1950 Jupiter-centered coordinates. Spacecraft Position (y) 8 105 ASCII_Real 24 %24.16e km y-component of the spacecraft position in EME 1950 Jupiter-centered coordinates. Sun Position (z) 9 129 ASCII_Real 24 %24.16e km z-component of the spacecraft position in EME 1950 Jupiter-centered coordinates. Spacecraft Velocity (x) 10 161 ASCII_Real 24 %24.16e km/s x-component of the spacecraft velocity in EME 1950 Jupiter-centered coordinates. Spacecraft Velocity (y) 11 185 ASCII_Real 24 %24.16e km/s y-component of the spacecraft velocity in EME 1950 Jupiter-centered coordinates. Spacecraft Velocity (z) 12 209 ASCII_Real 24 %24.16e km/s z-component of the spacecraft velocity in EME 1950 Jupiter-centered coordinates. Earth Position (x) 13 241 ASCII_Real 24 %24.16e km x-component of Earth position in EME 1950 Jupiter-centered coordinates. Earth Position (y) 14 265 ASCII_Real 24 %24.16e km y-component of Earth position in EME 1950 Jupiter-centered coordinates. Earth Position (z) 15 289 ASCII_Real 24 %24.16e km z-component of Earth position in EME 1950 Jupiter-centered coordinates. Earth Velocity (x) 16 321 ASCII_Real 24 %24.16e km/s x-component of Earth velocity in EME 1950 Jupiter-centered coordinates. Earth Velocity (y) 17 345 ASCII_Real 24 %24.16e km/s y-component of Earth velocity in EME 1950 Jupiter-centered coordinates. Earth Velocity (z) 18 369 ASCII_Real 24 %24.16e km/s z-component of Earth velocity in EME 1950 Jupiter-centered coordinates.