CZ-3B R/B, 44867

Orbit data source: Space-Track

CZ-3B R/B, 44867 is space debris in LEO originally from a launch on Mon, 16 Dec 2019 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
44867, 2019-090D
Orbit
LEO
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)
2019-12-16 (6 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: 5 hours ago

TLE from 5 hours ago
0 CZ-3B R/B
1 44867U 19090D   25300.14881470  .05353888  55842-5  43282-3 0  9992
2 44867  54.8106  25.3484 1552788 328.7314  22.9609 12.86075433111274
Epoch: 2025-10-27T03:34Z
TLE epoch observation values (Epoch: 2025-10-27T03:34:17.590Z)
Latitude
-0.00006°
Longitude
-63.97974°
Altitude
253.536 km
Speed
8.274 km/s
True Right ascension
01h 41m 23s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
04:21:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,512.045 km
Perigee altitude
122.221 km
Semi-major axis
7,695.27 km
Eccentricity
0.15528
Inclination
54.8106°
RAAN
25.3484°
Arg. of periapsis
328.7314°
True anomaly
31.36556°
Mean anomaly
22.9609°
Eccentric anomaly
26.99997°
Mean motion
3.2152 °/min
Orbital period
111.97 mins
BSTAR
0.00043282
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Other satellites on launch #90 in the year 2019 (2019-12-16 UTC)

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