Total Electron Content (TEC)

Definition status

This note defines Total Electron Content (TEC) as the line integral of electron density along the signal path between a GNSS satellite and a receiver. It is measured in TEC units (TECU), where 1 TECU = 10¹⁶ electrons/m².

Boundary:

  • This is an observable concept note, not a model or system-design note.
  • It does not cover algorithms for real-time SBAS ionospheric correction.
  • It links TEC to integrity, validation, and empirical studies in the vault.
  • It must not be used to publish operational GIVE, service-volume, availability, alerting, or procedure-eligibility claims without standards and service-provider evidence.

Working definition

TEC quantifies the total number of free electrons in a cylinder with a cross-sectional area of 1 m² along the propagation path. It directly determines the ionospheric delay experienced by GNSS signals through the dispersive nature of the ionospheric plasma.

TEC-to-delay conversion

At L1 frequency (1575.42 MHz):

TEC (TECU)Equivalent L1 delay (m)
10.162
101.62
508.10
10016.2
20032.4
341 (p99: Indonesian RO)55.4

Conversion formula:
delay_L1 = (40.3 × TEC) / f_L1²

Relationship to the vault

Parent domain

Sibling domains

  • SBAS Integrity — TEC uncertainty maps to ionospheric correction uncertainty, which impacts protection level and integrity risk
  • Protection Levels — large TEC gradients can inflate protection levels
  • Alert Limits — TEC anomalies may trigger integrity alerts

Implementation connection

TEC in SBAS context

Operational perspective

SBAS ground segments estimate ionospheric delay using dual-frequency ground receiver observations and broadcast corrections as gridded ionospheric vertical delays (GIVDs) or equivalent. The quality of these estimates determines:

  • User position accuracy — corrected versus uncorrected delay
  • Integrity risk — probability that the actual delay exceeds the broadcast bound (GIVE)
  • System availability — whether protection levels remain below alert limits

Empirical perspective

GNSS-RO provides an independent TEC measurement that can:

  1. Validate or invalidate empirical ionospheric models (e.g., IRI-2020)
  2. Quantify the tail of TEC delay distributions for threat-model design
  3. Characterize spatial TEC gradients that threaten differential correction accuracy

Critical boundary: GNSS-RO TEC measures a column along one ray path at one time. SBAS GIVE requires spatial interpolation over many ground-receiver IPPs. These are complementary, not interchangeable.

Current source anchors

Open provenance questions

  • What is the relationship between RO-derived TEC at a tangent point and the vertical IPP TEC used in SBAS grid interpolation?
  • Should TEC statistics from sparse RO sampling be treated as conservative (overbounding) or biased (undersampling tails)?
  • How do TEC conversion factors vary with geometry, receiver type, and signal frequency?

See also