CZ-3B R/B, 41587

Orbit data source: Space-Track

CZ-3B R/B, 41587 is space debris in HEO originally from a launch on Sun, 12 Jun 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
41587, 2016-037B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3C STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2016-06-12 (10 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.4 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 CZ-3B R/B
1 41587U 16037B   26295.72554771  .00076761 -12477-6  13130-2 0  9999
2 41587  19.4032 327.4438 5623981 100.8215 324.0027  4.72496867121564
Epoch: 2026-10-22T17:24Z
TLE epoch observation values (Epoch: 2026-10-22T17:24:47.322Z)
Latitude
-0.00003°
Longitude
35.08488°
Altitude
5,078.728 km
Speed
6.558 km/s
True Right ascension
21h 49m 45s
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
03:01:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
17,067.029 km
Perigee altitude
188.467 km
Semi-major axis
15,005.885 km
Eccentricity
0.5624
Inclination
19.4032°
RAAN
327.4438°
Arg. of periapsis
100.8215°
True anomaly
259.14888°
Mean anomaly
324.0027°
Eccentric anomaly
294.73636°
Mean motion
1.18073 °/min
Orbital period
304.9 mins
BSTAR
0.001313
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Other satellites on launch #37 in the year 2016 (2016-06-12 UTC)

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