CZ-3A R/B, 41435

Orbit data source: Space-Track

CZ-3A R/B, 41435 is space debris in HEO originally from a launch on Tue, 29 Mar 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
41435, 2016-021B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2016-03-29 (9 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.751 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CZ-3A R/B
1 41435U 16021B   25256.44615309 -.00000063  00000-0  00000-0 0  9999
2 41435  55.0944  53.5314 6626962 242.0433  37.3675  2.39503892 82352
Epoch: 2025-09-13T10:42Z
TLE epoch observation values (Epoch: 2025-09-13T10:42:27.626Z)
Latitude
0.00007°
Longitude
-99.81408°
Altitude
12,832.93 km
Speed
4.961 km/s
True Right ascension
03h 33m 55s
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
11:50:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
32,856.765 km
Perigee altitude
1,581.273 km
Semi-major axis
23,597.156 km
Eccentricity
0.6627
Inclination
55.0944°
RAAN
53.5314°
Arg. of periapsis
242.0433°
True anomaly
118.11552°
Mean anomaly
37.3675°
Eccentric anomaly
73.83625°
Mean motion
0.59876 °/min
Orbital period
601.24 mins
BSTAR
0
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Other satellites on launch #21 in the year 2016 (2016-03-29 UTC)

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