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 (11 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Double Cone, 2.1 m
Radar Cross Section
5.890 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago
0 YZ-1 R/B
1 41316U 16006B   26282.08638869  .00000036  00000-0  00000-0 0  9995
2 41316  56.3684  94.6023 1495361  76.9482 299.3355  1.60145526 62507
Epoch: 2026-10-09T02:04Z
TLE epoch observation values (Epoch: 2026-10-09T02:04:23.982Z)
Latitude
-0.00002°
Longitude
45.77206°
Altitude
22,810.84 km
Speed
3.794 km/s
True Right ascension
06h 18m 20s
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
20:02:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
29,096.178 km
Perigee altitude
19,866.906 km
Semi-major axis
30,859.679 km
Eccentricity
0.14954
Inclination
56.3684°
RAAN
94.6023°
Arg. of periapsis
76.9482°
True anomaly
283.11972°
Mean anomaly
299.3355°
Eccentric anomaly
291.35601°
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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