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, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-3B R/B
1 41587U 16037B   26171.28623260  .00019130  00000-0  75854-3 0  9994
2 41587  19.3889  90.4888 5664075 235.7970  57.2024  4.63029513115750
Epoch: 2026-06-20T06:52Z
TLE epoch observation values (Epoch: 2026-06-20T06:52:10.496Z)
Latitude
0.00008°
Longitude
78.92971°
Altitude
8,783.308 km
Speed
5.135 km/s
True Right ascension
06h 01m 54s
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
21:25:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
17,446.399 km
Perigee altitude
216.66 km
Semi-major axis
15,209.667 km
Eccentricity
0.56641
Inclination
19.3889°
RAAN
90.4888°
Arg. of periapsis
235.797°
True anomaly
124.21492°
Mean anomaly
57.2024°
Eccentric anomaly
89.65457°
Mean motion
1.15708 °/min
Orbital period
311.13 mins
BSTAR
0.00075854
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Other satellites on launch #37 in the year 2016 (2016-06-12 UTC)

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