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Link Budget

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Communication link analysis

Link budget calculator

Change any parameter and every result updates. Start from a band preset, then enter your own hardware figures.

Received power

-113.14dBm

-143.14 dBW

C/N0

58.47dB-Hz

SNR 14.49 dB in 25.0 kHz

Eb/N0

18.65dB

Required 9.59 dB

Link margin

9.06dB

Link closes with a healthy margin

Preset and carrier

1 W at 437 MHz into a 14 dBi crossed Yagi, 9.6 kbit/s BPSK. Representative values for teaching.

MHz
W

0.00 dBW, 30.00 dBm

Geometry

Where the satellite is relative to the station

km
°

Slant range used: 1,695.1 km

Antennas and losses

Transmit antenna

dBi

Receive antenna

dBi
dB
dB
dB
dB
dB
dB
dB

Receiver and requirement

Noise
K
kHz
kbit/s

9.60 kbit/s

BPSK needs 9.59 dB for BER 1e-5 without coding.

Budget

Each line adds to or subtracts from the carrier

Link budget lines
Transmit power0.00dBW
Transmit antenna gain0.00dBi
Transmit feeder loss-1.00dB
EIRP-1.00dBW
Free-space path loss-149.84dB
Atmospheric, rain, polarization, pointing, other-4.30dB
Receive antenna gain14.00dBi
Receive feeder loss-2.00dB
Received power-143.14dBW
Noise density N0 = kT-201.61dBW/Hz
Noise power N = kTB-157.63dBW
G/T-14.99dB/K
C/N058.47dB-Hz
SNR14.49dB
Eb/N018.65dB
Required Eb/N09.59dB
Margin9.06dB

Margin versus elevation

Satellite at 500 km, every other input fixed

Equations used

Wavelength
λ=cf\lambda = \dfrac{c}{f}
Free-space path loss (ITU-R P.525)
Lfs=20log⁡10 ⁣(4πdλ) dBL_{fs} = 20\log_{10}\!\left(\dfrac{4\pi d}{\lambda}\right)\ \text{dB}
Parabolic antenna gain
G=η(πDλ)2G = \eta\left(\dfrac{\pi D}{\lambda}\right)^{2}
Received power
Pr=Pt+Gt−Lt−Lfs−La+Gr−LrP_r = P_t + G_t - L_t - L_{fs} - L_a + G_r - L_r
Noise power
N=kTB,10log⁡10k=−228.6 dBW/K/HzN = kTB,\quad 10\log_{10}k = -228.6\ \text{dBW/K/Hz}
Signal to noise
CN0=Pr−10log⁡10(kT),EbN0=CN0−10log⁡10Rb\dfrac{C}{N_0} = P_r - 10\log_{10}(kT),\qquad \dfrac{E_b}{N_0} = \dfrac{C}{N_0} - 10\log_{10} R_b
Link margin
M=(EbN0)−(EbN0)reqM = \left(\dfrac{E_b}{N_0}\right) - \left(\dfrac{E_b}{N_0}\right)_{req}
Slant range from elevation
d=(Re+h)2−Re2cos⁡2ε−Resin⁡εd = \sqrt{(R_e + h)^2 - R_e^2\cos^2\varepsilon} - R_e\sin\varepsilon