Distance & Bearing Calculator

Calculate great circle distance and bearing between two airports or coordinates for precise flight planning and navigation.

Navigation Calculator

Departure Point

Destination Point

Wind Information (Optional)

Degrees (magnetic)
Knots
Knots (for ground speed calc)

Navigation Results

Great Circle Distance
True Bearing
Magnetic Bearing
Estimated variation:
Ground Speed
Wind Correction Angle
Heading to Fly
Flight Time
Reverse Bearing
From destination back to departure

Navigation Information

Great Circle Navigation

This calculator uses great circle navigation, which provides the shortest distance between two points on Earth's surface.

Magnetic Variation

Magnetic bearing is estimated using simplified variation models. For precise navigation, consult current aviation charts for exact magnetic variation.

Wind Triangle

Wind correction calculations assume constant wind conditions. Actual flight planning should account for varying winds aloft.

Popular Aviation Routes - Distance Reference

Reference distances for common flight routes worldwide. All distances are great circle (shortest path).

Route Distance (NM) Distance (km) True Bearing Typical Flight Time
KJFK → EGLL (New York - London) 3,459 6,406 051° 7h 00m
KLAX → PHNL (Los Angeles - Honolulu) 2,217 4,106 257° 5h 30m
EGLL → OMDB (London - Dubai) 2,994 5,545 107° 6h 45m
KSFO → RJTT (San Francisco - Tokyo) 4,476 8,290 306° 10h 30m
YSSY → KLAX (Sydney - Los Angeles) 6,516 12,066 057° 13h 30m
EDDF → KJFK (Frankfurt - New York) 3,364 6,231 288° 8h 30m
VHHH → WSSS (Hong Kong - Singapore) 1,401 2,595 214° 3h 50m
KATL → KMIA (Atlanta - Miami) 594 1,100 158° 1h 50m

* Flight times are estimates based on typical jet cruise speeds and assume favorable winds. Actual times vary with aircraft type, altitude, and wind conditions.

Great Circle vs. Rhumb Line Navigation

Great Circle Route

  • Shortest distance between two points
  • Saves fuel on long-distance flights
  • Used by airlines for oceanic routes
  • Requires changing heading continuously

Rhumb Line (Loxodrome)

  • Constant bearing (easier navigation)
  • Appears as straight line on Mercator charts
  • Practical for short-distance VFR flights
  • Longer distance than great circle route

Distance Difference Example: New York to London

Great Circle: 3,459 NM
Rhumb Line: 3,540 NM
Savings: 81 NM (2.3%)

Distance & Bearing Regulatory Requirements

FAA Requirements (United States)

14 CFR 91.103 - Preflight Action

Pilots must become familiar with all available information concerning the flight, including distances between waypoints and magnetic bearings for navigation planning.

14 CFR 61.51 - Pilot Logbooks

Requires accurate recording of cross-country flight distances, which must be calculated using great circle distance methods for flights over 50 nautical miles.

AC 61-23C - Pilot's Handbook of Aeronautical Knowledge

Provides guidance on navigation techniques, emphasizing the importance of accurate distance and bearing calculations for dead reckoning navigation.

EASA Requirements (Europe)

SERA.5005(f) - Pre-flight Action

Commanders must determine fuel requirements and alternate aerodromes, calculations requiring accurate distance measurements between airports.

FCL.935 - Cross-Country Flight Requirements

Defines cross-country flights as those using dead reckoning and radio navigation aids, requiring precise distance and bearing calculations.

Professional Navigation Applications

Flight Planning

  • Route distance calculations for fuel planning
  • Bearing determinations for dead reckoning
  • Waypoint navigation planning
  • Alternate airport assessments

In-Flight Navigation

  • Position fixing with two bearing lines
  • Great circle route optimization
  • Search and rescue coordinate systems
  • Emergency diversion calculations

Professional Best Practices

Coordinate Accuracy

  • Use precise GPS coordinates when available
  • Verify coordinates from official sources
  • Account for datum differences (NAD83 vs WGS84)
  • Double-check coordinate format entry

Navigation Planning

  • Calculate both magnetic and true bearings
  • Account for magnetic variation changes
  • Plan for great circle vs. rhumb line differences
  • Consider terrain and airspace constraints

Cross-Verification

  • Compare with sectional chart measurements
  • Verify against GPS flight planning systems
  • Cross-check with published airport distances
  • Validate against known reference points

Calculation Methodology

Haversine Formula (Distance)

a = sin²(Δφ/2) + cos φ₁ × cos φ₂ × sin²(Δλ/2)

c = 2 × atan2(√a, √(1−a))

d = R × c

Where φ is latitude, λ is longitude, R is Earth's radius (3,440.065 NM), and d is the distance.

Initial Bearing Formula

θ = atan2(sin Δλ × cos φ₂,

cos φ₁ × sin φ₂ − sin φ₁ × cos φ₂ × cos Δλ)

The result θ is the initial bearing from point 1 to point 2. Convert to compass bearing using (θ + 360) mod 360.

Wind Correction Angle

WCA = arcsin((Vw × sin(WD − TC)) / TAS)

Where Vw is wind speed, WD is wind direction, TC is true course, and TAS is true airspeed.

Ground Speed

GS = TAS × cos(WCA) + Vw × cos(WD − TC)

Ground speed calculation accounts for headwind/tailwind component along the track.