XW-4 (CAS-10), 54816 (Decayed)

Orbit data source: Public

XW-4 (CAS-10), 54816 was a payload satellite owned by CAMSAT (CN) that was launched on Thu, 29 Apr 2021 UTC via a CHANG ZHENG 7 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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/54816?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/54816?theme=dark&initialShowStats=false

Initial load time (optional)

TLE date request (optional)

Identifier	54816, 2021-035C
Orbit	Decayed
Last TLE update	Unknown
Origin	CAMSAT (CN / PRC)
Manufacturer	CAMSAT
Mission	Decayed Amateur Communications
Bus & Motor	CUBESAT 6U, Unknown motor
Mass	12 kg wet, 12 kg dry
Launch date (UTC)	2021-04-29 (4 years ago)
Launch vehicle	CHANG ZHENG 7
Launch site	Wenchang Satellite Launch Center (WSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 6 m
Radar Cross Section	0.410 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

Historical TLE search

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.

Orbital elements

Apogee altitude	Unknown
Perigee altitude	Unknown
Semi-major axis	Unknown
Eccentricity	Unknown
Inclination	Unknown
RAAN	Unknown
Arg. of periapsis	Unknown
True anomaly	Unknown
Mean anomaly	Unknown
Eccentric anomaly	Unknown
Mean motion	Unknown
BSTAR	Unknown
Orbital period	Unknown