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USA 396, 60322

Orbit data source: Public

USA 396, 60322 is a payload satellite owned by USSF SSC (US) that was launched on Tue, 30 Jul 2024 UTC via an ATLAS V 551 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/60322?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/60322?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

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ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

60322, 2024-134A

Orbit

Unknown

Last TLE update

Unknown

Origin

United States Space Force (US)

Manufacturer

Unknown (US)

Mission

Operational spacecraft

Bus & Motor

UNKNOWN, Unknown motor

Mass

~3,200 kg wet, 2,800 kg dry

Launch date (UTC)

2024-07-30 (9 months ago)

Launch vehicle

ATLAS V 551

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

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Historical TLE search

Format must be ISO8601 or YYYY-MM-DD

Definitive object data

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

True Right ascension

Unknown

True Declination

Unknown

Sunlit

N/A

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.