ARTEMIS.II

Orbital Flight Telemetry // Deep Space Network // Launch: April 1, 2026, 22:35:12 UTC

MISSION ELAPSED TIME
T+ 00D 00:00:00
UTC TIME
00:00:00
LOCAL TIME
00:00:00
LIVE STATUS
OUTBOUND COAST
VELOCITY
Velocity is calculated relative to the Earth's center of mass (Geocentric Reference Frame). This remains the primary metric for trans-lunar trajectory tracking in MCC-H.
0.00 KM/S
(0.00 MI/S)
DIST // EARTH
0 KM
(0 MI)
DIST // MOON
384,400 KM
(0 MI)
SIGNAL LATENCY
Due to the finite speed of light, there is a physical delay for signals traveling between Earth and Artemis II. Values represent a one-way transmission.
0.00 SEC
SYS_REF: X/Y_PLANAR
SCALE: 1:1.5M
COORD_SYS: J2000
NEXT MISSION MILESTONE
LOADING EVENT DATA...
EARTH MOON
LAUNCH
TLI
LUNAR FLYBY
RETURN
SPLASHDOWN
MISSION OBJECTIVES & PROGRESS 0.0%
MCC-H TERMINAL FEED

DISCLAIMER: DATA SOURCES INCLUDE OFFICIAL NASA TELEMETRY, EXTRAPOLATED MISSION MODELS, AND MATHEMATICAL SIMULATIONS.