artemis_ii

Stereo Stereo Baseline (deg) Crosseye Parallel

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 Apr 02 2026 02:09:20 UTC     JD 2461132.589815
 Wed Apr 01 2026 19:09:20 GMT-0700 (Pacific Daylight Time)
 Earth:24498 km (altitude)4.030 km/s
 Moon: 363332 km (altitude)3.231 km/s
 RA: 14 1 31 Dec: -15 22 12sky ω:53389 arcsec/hr
 

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Apr 02 2026 02:09:20 UTC

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Moon
Artemis II

Set time Date and Time (UTC)

Edit objects -- state vectors Object Reference object Name Color Shadow Label Trail Sub Z Mass Diameter Location (x,y,z) Velocity (x,y,z)

Edit objects -- orbital elements Object Reference object Name Color Shadow Label Trail Sub Z Mass Diameter a, e, i Ω, ω, MA

Look at

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Time step 1

Camera A Azimuth Altitude Distance Axes 3d Orbits Trails Names

Distance and speed Local time

Local time Wed Apr 01 2026 19:09:20 GMT-0700 (Pacific Daylight Time)

Coordinated Universal Time Thu Apr 02 2026 02:09:20 (UTC)

Julian Day 2461132.5898148147

Save as Simulation name: Keywords (optional) Description (optional) Author (optional) Share on orbitsimulator.com Create temporary link Your simulation is here: Source code:

Stars Star catalog

RA / Dec Boundaries Asterisms Star brightness Grid brightness RA spacing (min) Dec spacing (deg) Color

Globe Globe Cities USA state boundaries Europe boundaries South America boundaries

Rotating frame Target object A + Reference object A TL ML Longitude Altitude (AU) Distance (AU)

Cities A Latitude Longitude

Cities B Latitude Longitude

Frame A Target object A Camera object A Barycenter Minimum object size Trail size Zoom Stars Hip, Proper Static KBOs Orbits Phases Sun graphic Names Vertical lines

Frame B Target object B Camera object B Barycenter Minimum object size Trail size Zoom Stars Star labels Static KBOs Orbits Phases Sun graphic Labels

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Collision log

Simulation description

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Observatories - Paste astrometry here

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Screen shot

Screen shots Dimensions (x, y) Clear screen after screen shot Frame A foreground Frame A background Frame A position (x, y) Frame B foreground Frame B background Frame B position (x, y) 1 / 20 86400

Vectors

Distance and speed Tangential speed NaN Radial velocity NaN

Import object Importing -1024 -- Artemis II (spacecraft) (-1024) {source: Artemis_II_merged} Center body name: Sun (10)

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(JD, n)			2007 WD5
(e, q, tp)
(node, peri, i)

	e	q	tp	node	peri	i
e
q
tp
node
peri
i

Create objects

____Number_of_objects		Reference_object
Name
Red (0-255)
Green (0-255)
Blue (0-255)
Radius
Mass
Semi-major axis
Eccentricity
Inclination (deg)
Ω Longitude(deg)
ω Periapsis(deg)
MA (deg)

Override	Top	Left	Height	Width
Perspective A	Top	Left	Height	Width
Perspective B	Top	Left	Height	Width

Earth:	24498 km (altitude)	4.030 km/s
Moon:	363332 km (altitude)	3.231 km/s