YZ-1 R/B, 41316

Orbit data source: Space-Track

YZ-1 R/B, 41316 is space debris originally from a launch on Mon, 01 Feb 2016 UTC launched from the Xichang Space Center, China (XSC). 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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Identifier
41316, 2016-006B
Orbit
Active
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
YZ-1, Unknown motor
Mass
~2,075 kg wet, ~2,075 kg dry
Launch date (UTC)
2016-02-01 (10 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Double Cone, 2.0 m
Radar Cross Section
5.890 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 YZ-1 R/B
1 41316U 16006B   26170.31488779 -.00000017  00000-0  00000-0 0  9990
2 41316  56.2892  97.3881 1472177  75.7281 300.0828  1.60145481 60719
Epoch: 2026-06-19T07:33Z
TLE epoch observation values (Epoch: 2026-06-19T07:33:26.305Z)
Latitude
0.00001°
Longitude
76.48587°
Altitude
22,751.5 km
Speed
3.802 km/s
True Right ascension
06h 29m 33s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:24:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
29,024.643 km
Perigee altitude
19,938.459 km
Semi-major axis
30,859.688 km
Eccentricity
0.14722
Inclination
56.2892°
RAAN
97.3881°
Arg. of periapsis
75.7281°
True anomaly
284.21609°
Mean anomaly
300.0828°
Eccentric anomaly
292.27744°
Mean motion
0.40036 °/min
Orbital period
899.18 mins
BSTAR
0
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Other satellites on launch #6 in the year 2016 (2016-02-01 UTC)

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