Earth & Satellite — Keplerian Orbit

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Telemetry

Orbit class—

Sim time0 s

Orbital Elements

Semi-major a—

Eccentricity e—

Inclination i—

RAAN Ω—

Arg. perigee ω—

Period T—

Perigee alt.—

Apogee alt.—

Live State

Altitude r-R⊕—

Speed |v|—

True anom. ν—

Mean anom. M—

Earth

Axial tilt (ε)—

Sidereal spin—

Sun

Distance—

Angular size—

Light time—

Position vector r⃗ (ECI, km)

x—

y—

z—

|r|—

Orbit Parameters

Semi-major axis a — 8000 km Eccentricity e — 0.10 Inclination i — 45° RAAN Ω — 0° Arg. of perigee ω — 0° Time scale — 100×

Axis & obliquity r⃗ / v⃗ vectors

Two-body (Kepler) propagation · real Earth constants (GM, R⊕)