CZ-3B R/B, 49331

Orbit data source: Space-Track

CZ-3B R/B, 49331 is space debris in HEO originally from a launch on Sun, 24 Oct 2021 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
49331, 2021-094B
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)
2021-10-24 (5 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: 2 days ago

TLE from 2 days ago
0 CZ-3B R/B
1 49331U 21094B   26259.88656264  .00000241  00000-0  55505-3 0  9995
2 49331  28.3042  82.2807 7113243 223.1616  51.5817  2.45423914 42715
Epoch: 2026-09-16T21:16Z
TLE epoch observation values (Epoch: 2026-09-16T21:16:39.012Z)
Latitude
-0.00018°
Longitude
127.27151°
Altitude
17,447.027 km
Speed
4.036 km/s
True Right ascension
05h 29m 03s
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
02:35:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,358.482 km
Perigee altitude
324.857 km
Semi-major axis
23,219.806 km
Eccentricity
0.71132
Inclination
28.3042°
RAAN
82.2807°
Arg. of periapsis
223.1616°
True anomaly
136.93986°
Mean anomaly
51.5817°
Eccentric anomaly
92.30462°
Mean motion
0.61342 °/min
Orbital period
586.88 mins
BSTAR
0.00055505
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Other satellites on launch #94 in the year 2021 (2021-10-24 UTC)

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