ORBITAL // Vector Flight Console

Flight Data

BODYEARTH

ALTITUDE—

VELOCITY—

APOAPSIS—

PERIAPSIS—

Orbit

ECCENTRICITY—

INCLINATION—

PERIOD—

TO AP / TO PE— / —

STATUSGO

Orbit Ops

GUIDANCEMANUAL

Vehicle

CRAFTCSM+LM

SASOFF

ENGINEIDLE

ΔV REMAINING—

THR

100%

SPS

100%

RCS

100%

TGT DIST / RVEL— / —

Maneuver Node — [N]

STATENO NODE

ΔV TOTAL0 m/s

TIG T−—

BURN EST—

ALIGN ERR—

PRED AP / PE— / —

TIG

PRO +0

NRM +0

RAD +0

Mission

Controls — [H] to hide

W/S A/D Q/Epitch / yaw / roll I/K J/L U/ORCS translate SPACEfire engine SHIFT / CTRLthrottle ± (Z max, X cut) TSAS (kill rotation) N / Bmaneuver node / execute burn Vswap CSM ↔ LM (when separated) [ ] / { }node ΔV / node TIG Mmap view , / .time warp − / + Rreset flight MOUSEorbit camera / wheel zoom