YZ-2 R/B, 41840

Orbit data source: Space-Track

YZ-2 R/B, 41840 is space debris in GEO originally from a launch on Thu, 03 Nov 2016 UTC launched from the Wenchang Satellite Launch Center (WSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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YZ-2 R/B details

Identifier	41840, 2016-065C
Orbit	GEO
Last TLE update	1 day ago
Origin	CNSA (CN / PRC)
Manufacturer	CALT
Mission	Spacecraft
Bus & Motor	YZ-2, Unknown motor
Mass	~2,000 kg wet, ~2,000 kg dry
Launch date (UTC)	2016-11-03 (8 years ago)
Launch vehicle	Unknown
Launch site	Wenchang Satellite Launch Center (WSC)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 4 m
Radar Cross Section	17.609 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 YZ-2 R/B
1 41840U 16065C   24360.27032806 -.00000100  00000-0  00000-0 0  9990
2 41840   7.9242  72.3286 0478361 217.9937 138.3999  0.93473464 27818

Epoch: 2024-12-25T06:29Z

Definitive object data (Epoch: 2024-12-25T06:29:16.344Z)

Latitude	-0.00001°
Longitude	-119.38362°
Altitude	39,439.408 km
Speed	2.895 km/s
True Right ascension	04h 48m 48s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	7.35665°
Longitude	-51.76353°
Altitude	39,619.301 km
Speed	2.883 km/s
Apparent Right ascension	08h 58m 29s
Apparent Declination	2° 25' 34"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	12:48:39
Azimuth	249.714° W
Elevation	26.005°
Doppler factor	1

Orbital elements

Apogee altitude	39,921.699 km
Perigee altitude	35,694.314 km
Semi-major axis	44,186.144 km
Eccentricity	0.0478361
Inclination	7.9242°
RAAN	72.3286°
Arg. of periapsis	217.9937°
True anomaly	141.88114°
Mean anomaly	138.3999°
Eccentric anomaly	140.15594°
Mean motion	0.23368 °/min
BSTAR	Unknown
Orbital period	1540.59 mins