EE 499 — Satellite Technologies · prototype tool

Orbit & Ground-Track Visualizer

One satellite, a two-body Keplerian model, and a live eccentricity control. The 3D view shows the inertial orbit around a rotating Earth; the map below shows where the satellite is directly overhead.

3D orbit — Earth-centred inertial

Drag to rotate · scroll to zoom

Ground track — Earth-fixed

Bold = current revolution · faded = earlier revolutions

Semi-major axis
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Eccentricity
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Inclination
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Orbital period
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Perigee altitude
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Apogee altitude
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Current altitude
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Current speed
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Latitude
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Longitude
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Elapsed (simulated)
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Revolutions
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Try this in class

  1. Start at e = 0. Speed is constant and the track is a clean sinusoid.
  2. Raise e to about 0.2 — the ellipse appears and the speed readout starts to breathe.
  3. Push e to 0.6 or more. The satellite whips through perigee and crawls near apogee.
  4. Change inclination — the track's latitude limits follow it (±i, or ±180°−i above 90°).
  5. Let it run for several revolutions: each pass shifts west because the Earth turned underneath.
  6. Load Molniya-like and watch the long northern dwell that a circular orbit cannot give.