XJS B, 43519 (Decayed)

Orbit data source: Space-Track

XJS B, 43519 was a payload satellite owned by PLA SSF (CN) in LEO that was launched on Wed, 27 Jun 2018 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). Payloads include a variety of satellites, spacecraft, and rockets 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

XJS B details

Identifier	43519, 2018-054B
Orbit	Decayed
Last TLE update	1 month ago
Origin	PLA SSF (CN / PRC)
Manufacturer	SECM
Mission	Decayed Civil Technology
Bus & Motor	Unknown
Mass	~500 kg wet, ~500 kg dry
Launch date (UTC)	2018-06-27 (7 years ago)
Launch vehicle	CHANG ZHENG 2C
Launch site	Xichang Space Center, China (XSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 1 m
Radar Cross Section	0.446 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month ago

0 XJS B
1 43519U 18054B   24317.76559676  .28406718  14471-5  81980-3 0  9995
2 43519  35.0060 159.8307 0006738 296.7770 161.4008 16.45174755358149

Epoch: 2024-11-12T18:22Z

Definitive object data (Epoch: 2024-11-12T18:22:27.56Z)

Latitude	34.75071°
Longitude	-68.16548°
Altitude	156.676 km
Speed	7.816 km/s
True Right ascension	17h 19m 17s
True Declination	34° 34' 30"
Sunlit	Object was in daylight at TLE epoch

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	159.896 km
Perigee altitude	151.091 km
Semi-major axis	6,533.63 km
Eccentricity	0.0006738
Inclination	35.006°
RAAN	159.8307°
Arg. of periapsis	296.777°
True anomaly	161.42541°
Mean anomaly	161.4008°
Eccentric anomaly	161.41311°
Mean motion	4.10971 °/min
BSTAR	0.0008198
Orbital period	87.6 mins