DECAYED

ARTEMIS 2 (INTEGRITY), 68538 (Decayed)

Artemis II builds on the success of the uncrewed Artemis I in 2022, and demonstrates a broad range of capabilities needed on deep space missions. The Artemis II test flight is NASA’s first mission with crew aboard the SLS (Space Launch System) rocket and Orion spacecraft. Following Artemis II, the Artemis III mission, now in 2027, will be designed to test out systems and operational capabilities in low Earth orbit to prepare for an Artemis IV moon landing in 2028.

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<iframe src="https://www.satcat.com/sats-embedded/68538?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/68538?theme=dark&initialShowStats=false

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Embedded visualization by NASA

Identifier

68538, 2026-069A

Orbit

Decayed

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

LM KSC

Mission

Decayed Human Exploration

Bus & Motor

ORION, Unknown motor

Mass

25,848 kg wet, 9,400 kg dry

Launch date (UTC)

2026-04-01 (2 weeks ago)

Launch vehicle

SLS BLOCK 1

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cone, 4.0 m

Radar Cross Section

13.354 m²

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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ARTEMIS 2 (INTEGRITY) Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
399 mins	2026-04-13 06:17:35.628Z	134.022° SE	2026-04-13 09:38:35.628Z	179.913° S	23.351°	2026-04-13 12:56:35.628Z	225.053° WSW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in descending order

CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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ARTEMIS 2 (INTEGRITY), 68538 (Decayed)

ARTEMIS 2 (INTEGRITY) Visibility forecast

Co-orbital & Co-planar RSOs

Documentation