Satellite Communications and Space Practical Satcom Questions Informational

How do I calculate the look angle and azimuth from a ground station to a geostationary satellite?

Calculating the look angle (elevation) and azimuth from a ground station to a geostationary satellite requires the ground station's latitude and longitude and the satellite's orbital longitude. The satellite is in a geostationary orbit at 35,786 km altitude above the equator at a specific longitude. The calculation uses: Step 1: Calculate the relative longitude: delta_L = satellite_longitude - station_longitude (positive if the satellite is east of the station). Step 2: Calculate the elevation angle: el = arctan((cos(delta_L) × cos(lat) - 0.1513) / sqrt(1 - cos^2(delta_L) × cos^2(lat))), where lat is the ground station latitude and the 0.1513 factor is the Earth radius / orbit radius ratio (6378/42164). Step 3: Calculate the azimuth: intermediate: X = arctan(tan(delta_L) / sin(lat)). If the station is in the northern hemisphere: azimuth = 180 + X (if delta_L is positive, satellite is east) or azimuth = 180 - X (if delta_L is negative, satellite is west). For the southern hemisphere: azimuth = 360 - X or azimuth = X (depending on the satellite's relative position). Example: Ground station at 28.5°N, 80.5°W (Cape Canaveral). Satellite at 97°W (e.g., Galaxy 19). delta_L = -97 - (-80.5) = -16.5°. Elevation approximately 47.5°. Azimuth approximately 207° (southwest).
Category: Satellite Communications and Space
Updated: April 2026
Product Tie-In: LNBs, BUCs, Antennas, Tracking Systems

Satellite Look Angle Calculation

The look angle and azimuth calculation is the first step in pointing a satellite dish. These angles tell the installer exactly where to aim the antenna.

ParameterGEOMEOLEO
Altitude35,786 km2,000-35,786 km200-2,000 km
Latency (one-way)~270 ms50-150 ms1-20 ms
Coverage per SatFull hemisphereRegionalLocal footprint
HandoverNonePeriodicFrequent
Path Loss (Ku-band)~206 dB190-206 dB170-190 dB
  • Performance verification: confirm specifications against the application requirements before finalizing the design
  • Environmental factors: temperature range, humidity, and vibration affect long-term reliability and parameter drift
  • Cost vs. performance: evaluate whether the application demands premium components or standard commercial grades
  1. Interface compatibility: verify impedance, connector type, and mechanical form factor match the system architecture
  2. Margin allocation: include sufficient design margin to account for manufacturing tolerances and aging effects
Common Questions

Frequently Asked Questions

What tools calculate look angles?

Online calculators: DishPointer.com: enter your address and satellite; shows the azimuth, elevation, and a Google Maps overlay of the pointing direction. SatLex: European satellite look angle calculator. LyngSat: satellite database with look angle tools. Smartphone apps: SatFinder, Dish Align: use the phone's GPS, compass, and accelerometer to point the dish in real-time. For professional installations: the antenna controller software (Andrew/CommScope ACU, AvL Technologies interface) computes the look angles and drives the antenna automatically.

How accurate must the pointing be?

The required pointing accuracy depends on the antenna beamwidth: for a 1.2 m Ku-band dish (beamwidth approximately 1.5°): pointing accuracy must be better than ±0.5° (1/3 of the beamwidth). For a 3.7 m C-band dish (beamwidth approximately 1.2°): accuracy better than ±0.3°. For a 60 cm Ku-band dish (beamwidth approximately 3°): accuracy better than ±1°. A 1° pointing error on a 1.5° beamwidth antenna causes approximately 3 dB signal loss. At the installation: fine-tune the pointing by peaking the received signal strength on a known satellite beacon.

What about non-geostationary satellites?

Non-GEO satellites (LEO, MEO, HEO) require real-time tracking: the satellite moves across the sky, so the antenna must continuously update its pointing angles. The look angles are calculated from: the satellite's orbital elements (TLE: Two-Line Element set), the current time, and the ground station position. Software: STK (Systems Tool Kit), GPredict, Orbitron compute the trajectory and look angles in real-time. Tracking antennas: use a computer-controlled positioner to follow the satellite across the sky.

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