Skip to main content
The Standard Product 3 (SP3) format is an ASCII standard developed by the International GNSS Service (IGS) for distributing satellite orbit and clock correction data. Originally designed for GPS satellites, SP3-c (the current version) supports multiple GNSS constellations and LEO satellites, making it widely used for precise orbit ephemerides.

Key Components

An SP3 file contains several distinct sections:
  • Header: 22 lines of file-level metadata including version, time system, coordinate frame, satellite list, and accuracy information
  • Comments: 4 optional comment lines for additional documentation
  • Epoch Blocks: Repeating blocks containing position/clock records and optional velocity/correlation records
  • EOF Marker: End-of-file indicator

File Structure Overview

Header Lines (1-22)
├── Line 1: Version, start time, epochs, coordinate system, orbit type
├── Line 2: GPS week, seconds of week, epoch interval, MJD
├── Lines 3-7: Satellite identifiers (up to 85 satellites)
├── Lines 8-12: Orbit accuracy exponents
├── Line 13: File type and time system
├── Lines 15-16: Standard deviation base values
└── Lines 19-22: Comments

Data Section
├── Epoch Header (* YYYY MM DD HH MM SS.ssssssss)
├── Position Records (P)
├── Position Correlation Records (EP) [optional]
├── Velocity Records (V) [optional]
└── Velocity Correlation Records (EV) [optional]

EOF

Header Fields

Line 1: File Identification

ColumnsFieldDescription
1-2Version#c for SP3-c format
3P/V FlagP = position only, V = position and velocity
4-31Start TimeYear, month, day, hour, minute, second
33-39EpochsNumber of epochs in file
41-45Data UsedMeasurement type descriptor (e.g., ORBIT)
47-51Coordinate SystemReference frame (e.g., ITR14, IGS14)
53-55Orbit TypeFIT, EXT, BCT, or HLM
57-60AgencyProducing agency identifier

Line 2: Time Reference

ColumnsFieldDescription
4-7GPS WeekGPS week number
9-23Seconds of Week0.0 to 604800.0
25-38Epoch IntervalTime between epochs (seconds)
40-44MJDModified Julian Day at start
46-60Fractional DayDecimal fraction of day

Lines 3-7: Satellite Identifiers

Up to 85 satellites listed across 5 lines (17 per line). Each satellite uses a system identifier:
LetterSystem
GGPS
RGLONASS
EGalileo
CBeiDou/COMPASS
JQZSS
LLEO satellites

Line 13: File Type and Time System

ColumnsFieldValues
4-5File TypeG (GPS), R (GLONASS), M (mixed), L (LEO), E (Galileo), C (COMPASS), J (QZSS)
10-12Time SystemGPS, GLO, GAL, TAI, UTC, QZS

Data Records

Position and Clock Record (P)

P G01  15000.123456  -5000.654321  20000.987654    123.456789  1  2  3  10
ColumnsFieldUnits
1Record TypeP
2-4Satellite IDSystem letter + PRN
5-18X Positionkilometers
19-32Y Positionkilometers
33-46Z Positionkilometers
47-60Clock Correctionmicroseconds
62-63X Std Dev Exponent2^nn mm
65-66Y Std Dev Exponent2^nn mm
68-69Z Std Dev Exponent2^nn mm
71-73Clock Std Dev Exponent2^nn ps
Bad or absent position values are set to 0.000000. Bad or absent clock values are set to 999999.999999.

Optional Flags (Position Record)

ColumnFlagMeaning
75Clock EventE = discontinuity, blank = normal
76Clock PredictionP = predicted, blank = observed
79ManeuverM = orbit maneuver, blank = normal
80Orbit PredictionP = predicted, blank = observed

Velocity and Clock Rate Record (V)

Only present when Line 1 P/V flag is V:
ColumnsFieldUnits
1Record TypeV
2-4Satellite IDSystem letter + PRN
5-18X Velocitydecimeters/second
19-32Y Velocitydecimeters/second
33-46Z Velocitydecimeters/second
47-60Clock Rate10^-4 microseconds/second

Correlation Records (EP, EV)

Optional high-precision correlation records provide:
  • Standard deviations in physical units (mm for position, mm/s for velocity)
  • Six correlation coefficients (xy, xz, xc, yz, yc, zc) scaled by 10^7

Supported Time Systems

CodeTime System
GPSGPS Time
GLOGLONASS UTC
GALGalileo System Time
TAIInternational Atomic Time
UTCCoordinated Universal Time
QZSQZSS Time
All times in an SP3 file use the SAME time system, whether expressed as Gregorian dates or Modified Julian Dates.

Common Use Cases

  • Precise Point Positioning (PPP): High-accuracy GNSS positioning using precise orbits
  • Orbit Comparison: Validating orbit determination results against IGS products
  • LEO Satellite Tracking: Distributing precise orbits for Earth observation satellites
  • Clock Analysis: Satellite clock characterization and time transfer
  • Geodetic Research: Reference frame determination and geophysical studies

Sample SP3-c File

#cP2024 12 15  0  0  0.00000000      96 ORBIT IGS14 FIT  IGS
## 2341 518400.00000000   900.00000000 60658 0.0000000000000
+   32   G01G02G03G04G05G06G07G08G09G10G11G12G13G14G15G16G17
+        G18G19G20G21G22G23G24G25G26G27G28G29G30G31G32  0  0
+          0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0
+          0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0
+          0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0
++         2  2  2  2  2  2  2  2  2  2  2  2  2  2  2  2  2
++         2  2  2  2  2  2  2  2  2  2  2  2  2  2  2  0  0
++         0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0
++         0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0
++         0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0  0
%c G  cc GPS ccc cccc cccc cccc cccc ccccc ccccc ccccc ccccc
%c cc cc ccc ccc cccc cccc cccc cccc ccccc ccccc ccccc ccccc
%f  1.2500000  1.025000000  0.00000000000  0.000000000000000
%f  0.0000000  0.000000000  0.00000000000  0.000000000000000
%i    0    0    0    0      0      0      0      0         0
%i    0    0    0    0      0      0      0      0         0
/* IGS FINAL ORBIT COMBINATION FROM WEIGHTED AVERAGE OF:
/* cod emr esa gfz grg jpl mit ngs sio
/* REFERENCED TO IGS TIME (IGST) AND target/IGS14
/* CLK ANT Z-OFFSET (M): II/IIA 1.023; IIR 0.000
*  2024 12 15  0  0  0.00000000
PG01  15234.123456  -8234.654321  19876.987654    123.456789
PG02  12456.789012   5678.901234  22345.678901    -45.678901
PG03  -8765.432109  18765.432109  14567.890123    234.567890
EOF

Technical References