XJS D, 45250 (Decayed)

Orbit data source: Space-Track

XJS D, 45250 was a payload satellite owned by SAST (CN) in LEO that was launched on Wed, 19 Feb 2020 UTC via a CHANG ZHENG 2D 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 D details

Identifier	45250, 2020-014B
Orbit	Decayed
Last TLE update	7 months ago
Origin	SAST (CN / PRC)
Manufacturer	SAST
Mission	Decayed Civil Technology
Bus & Motor	Unknown
Mass	~200 kg wet, ~200 kg dry
Launch date (UTC)	2020-02-19 (5 years ago)
Launch vehicle	CHANG ZHENG 2D
Launch site	Xichang Space Center, China (XSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, Unknown HBR
Radar Cross Section	0.446 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 XJS D
1 45250U 20014B   24156.12265476  .47187354  14195-5  59950-3 0  9999
2 45250  34.9979  65.9969 0002919 264.0659 236.7954 16.49520532241477

Epoch: 2024-06-04T02:56Z

Definitive object data (Epoch: 2024-06-04T02:56:37.371Z)

Latitude	21.32673°
Longitude	-84.87711°
Altitude	140.152 km
Speed	7.826 km/s
True Right ascension	14h 09m 18s
True Declination	21° 11' 58"
Sunlit	Object was in full shadow 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	145.93 km
Perigee altitude	142.122 km
Semi-major axis	6,522.163 km
Eccentricity	0.0002919
Inclination	34.9979°
RAAN	65.9969°
Arg. of periapsis	264.0659°
True anomaly	236.76742°
Mean anomaly	236.7954°
Eccentric anomaly	236.78141°
Mean motion	4.12055 °/min
BSTAR	0.0005995
Orbital period	87.37 mins