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 (10 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
32.704 m², Large (>1 m²)

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

TLE from 2 weeks ago
0 CZ-3A R/B
1 41435U 16021B   26157.80799416 -.00000146  00000-0  00000-0 0  9994
2 41435  55.0308   2.1331 6670266 271.0967  19.1874  2.39503379 88732
Epoch: 2026-06-06T19:23Z
TLE epoch observation values (Epoch: 2026-06-06T19:23:30.695Z)
Latitude
-0.00018°
Longitude
176.06045°
Altitude
6,556.169 km
Speed
6.689 km/s
True Right ascension
00h 08m 37s
True Declination
0° 00' 01"
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
23:27:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
32,959.017 km
Perigee altitude
1,479.102 km
Semi-major axis
23,597.196 km
Eccentricity
0.66703
Inclination
55.0308°
RAAN
2.1331°
Arg. of periapsis
271.0967°
True anomaly
88.77109°
Mean anomaly
19.1874°
Eccentric anomaly
47.25292°
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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