Specific Product Header for GPSX_RO_1B and GPS_RN_1B products
id | field name | definition |
0 | SPH_Descriptor |
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1 | Orbit_Information |
xml record |
id | field name | definition |
0 | Sensing_Start |
xml time |
UTC start time of sensing
unit: "s since 2000-01-01"
value: if(length(.) == 0, nan, if(str(., 30) == "UTC=9999-99-99T99:99:99.999999", +inf, if(str(., 30) == "UTC=0000-00-00T00:00:00.000000", -inf, time(str(.), "'UTC='yyyy-MM-dd'T'HH:mm:ss.SSSSSS"))))
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1 | Sensing_Stop |
xml time |
UTC stop time of sensing
unit: "s since 2000-01-01"
value: if(length(.) == 0, nan, if(str(., 30) == "UTC=9999-99-99T99:99:99.999999", +inf, if(str(., 30) == "UTC=0000-00-00T00:00:00.000000", -inf, time(str(.), "'UTC='yyyy-MM-dd'T'HH:mm:ss.SSSSSS"))))
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2 | Maneuver_Information |
xml record |
id | field name | definition |
0 | Maneuver_Id |
xml array[dim_0] |
dim_0: determined automatically from xml file
ascii int16 | size: 3 |
Maneuver identification code
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3 | Ephemeris_Information |
xml record |
id | field name | definition |
0 | Mass_SC |
ascii float |
Mass of the space craft at start of the product
unit: "kg"
attribute: unit |
ascii string | size: 2 |
fixed value: "kg"
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available: optional
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1 | r_CoG_ARP |
ascii array[3] |
Vector from S/C center of gravity to antenna reference point, S/C frame
attribute: unit |
ascii string | size: 1 |
fixed value: "m"
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available: optional
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2 | RINEX_Filename |
xml string |
Suggested name of RINEX file. Eg. ssssdddhmm.yyO
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4 | Product_Confidence_Data |
xml record |
id | field name | definition |
0 | Quality_Indicator |
ascii int16 | size: 3 |
General product quality indicator
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1 | HK_ISP_Missing |
ascii uint32 | size: 5 |
Number of missing/erroneous platform HK ISPs
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2 | GPSR_ISP_Missing |
ascii uint32 | size: 5 |
Number of missing/erroneous GPSR ISPs
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3 | STR_ISP_Missing |
ascii uint32 | size: 5 |
Number of missing/erroneous STR ISPs
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5 | List_of_DSDs |
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