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LONGJIANG 1, 43471

Orbit data source: Public

LONGJIANG 1, 43471 is a Chinese payload satellite that was launched on Sun, 20 May 2018 UTC via a CHANG ZHENG 4C launch vehicle from the Xichang Space Center, China (XSC). 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.

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Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/43471?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/43471?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

43471, 2018-045B

Orbit

Unknown

Last TLE update

Unknown

Origin

China Aerospace Science and Technology Corporation (CASC) (CN / PRC)

Manufacturer

Harbin

Mission

Non-operational Civil Planetary

Bus & Motor

DSLWP, Unknown motor

Mass

45 kg wet, 45 kg dry

Launch date (UTC)

2018-05-20 (7 years ago)

Launch vehicle

CHANG ZHENG 4C

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Pan + 4 Ant, 0.5 m

Radar Cross Section

0.325 m²

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TLE epoch observation values

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.