ISR University COE Orbital Elements Lab
ISR University · Orbit Lab
New to Orbit Lab? Build a satellite’s orbit and watch it fly in real time.• Start from a preset (LEO, GEO, Molniya…) or set the six orbital elements — a, e, i, Ω, ω, ν — with the sliders, or type exact values.• Switch between the 3D globe and the 2D groundtrack with the buttons just below.• Press Play to animate the orbit and watch the live stats in the readouts panel on the right.• Save a labeled snapshot anytime with Export image.
Orbit size
Orbital elements
Semi-major axis (a)
Eccentricity (e)
Inclination (i)
RAAN (Ω)
Argument of perigee (ω)
True anomaly (ν)
Reference toggles
Presets
Animation
Speed1.0×
Typed value support: eccentricity accepts typed numeric values; inclination, RAAN, argument of perigee, and true anomaly accept typed values to 0.1° while preserving slider control.
Readouts
Period
Perigee alt.
Apogee alt.
Current alt.
Current speed
Subsatellite--
Sim elapsed00:00:00
Sim UTC
Legend
Orbit path
Ascending node
Descending node
Perigee
Apogee
Vernal equinox

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