Mission geometry
Doppler and Propagation Delay Tool
Separate carrier frequency shift from geometric signal flight time.
Enter the design inputs, then calculate to inspect the results.
Swipe the diagram sideways to see the full view. With a keyboard, focus the diagram and use the arrow keys.
LEO overhead pass
Circular orbit above a fixed station on a non-rotating spherical Earth. This is a teaching model, not a real satellite tracker.
Radial velocity 0.0 m/s · Doppler 0.0 Hz · orbital speed 7455.5 m/s
At zenith radial velocity is zero while orbital speed is not. Uses the carrier frequency and constant mode selected above. Independent pass controls do not replace your entered radial velocity. Earth rotation, inclined/off-centre passes, drag and refraction are excluded.
Understand the system
Signed Doppler shift
A LEO satellite approaching a station raises received carrier frequency; recession lowers it. Use radial velocity along the line of sight, not total orbital speed. Here positive v_r means recession; the first-order approximation applies when speed is much smaller than c.
f_c: Hz; v_r: m/s, positive receding; c: m/s; Δf: Hz.
A faster carrier produces a larger Doppler shift for the same radial speed.
Source: finalExam.pdf · PDF page 1
Common mistakes
- Convert km/s to m/s when c is m/s.
- One slant range is not a full ground-to-ground relay path.
- Do not assume orbital speed equals radial speed.
Formula reference and symbol definitions
First-order Doppler
f_c: Hz; v_r,c: m/s
v_r positive receding; |v_r| much smaller than c.
Example: At 2 GHz and recession velocity +6000 m/s, Δf = −2 × 10⁹ × 6000/(3 × 10⁸) = −40000 Hz.
Open related tool →Propagation delay
d: m; c: m/s; t: s
Geometric flight time only.
Example: A 36000 km path gives t = 36 × 10⁶/(3 × 10⁸) = 0.120 s one way.
Open related tool →