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QUEQIAO, 43470

Orbit data source: Public

QUEQIAO, 43470 is a payload satellite owned by CASC (CN) 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/43470?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/43470?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

43470, 2018-045A

Orbit

Unknown

Last TLE update

Unknown

Origin

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

Manufacturer

CAST

Mission

Operational Civil Planetary

Bus & Motor

CAST-100, 130N LAE

Mass

425 kg wet, 325 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 + 2 Pan + 1 Dish, 4.2 m

Radar Cross Section

5.222 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.