XJS E, 45251 (Decayed)

Orbit data source: Space-Track

XJS E, 45251 was a payload satellite owned by Harbin (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 E details

Identifier	45251, 2020-014C
Orbit	Decayed
Last TLE update	9 months ago
Origin	Harbin (CN / PRC)
Manufacturer	Harbin
Mission	Decayed Civil Technology
Bus & Motor	Unknown
Mass	500 kg wet, 500 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 9 months ago

0 XJS E
1 45251U 20014C   24100.53376843  .08568485  13520-5  71805-3 0  9994
2 45251  35.0216  36.8737 0007634 230.7084 292.0228 16.38395432233146

Epoch: 2024-04-09T12:48Z

Definitive object data (Epoch: 2024-04-09T12:48:37.592Z)

Latitude	9.87286°
Longitude	172.16361°
Altitude	166.311 km
Speed	7.811 km/s
True Right ascension	13h 30m 18s
True Declination	9° 48' 35"
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	178.484 km
Perigee altitude	168.481 km
Semi-major axis	6,551.62 km
Eccentricity	0.0007634
Inclination	35.0216°
RAAN	36.8737°
Arg. of periapsis	230.7084°
True anomaly	291.94167°
Mean anomaly	292.0228°
Eccentric anomaly	291.98224°
Mean motion	4.0928 °/min
BSTAR	0.00071805
Orbital period	87.96 mins