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: 14 hours ago

TLE from 14 hours ago
0 CZ-3B R/B
1 44867U 19090D   25258.98954557  .01552923  19998-5  26196-3 0  9997
2 44867  54.8517 132.4294 2423020 267.6846  64.7294 10.90893602106465
Epoch: 2025-09-15T23:44Z
TLE epoch observation values (Epoch: 2025-09-15T23:44:56.737Z)
Latitude
0.00007°
Longitude
141.00676°
Altitude
1,789.448 km
Speed
7.157 km/s
True Right ascension
08h 49m 43s
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
06:48:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,290.449 km
Perigee altitude
128.789 km
Semi-major axis
8,587.756 km
Eccentricity
0.2423
Inclination
54.8517°
RAAN
132.4294°
Arg. of periapsis
267.6846°
True anomaly
92.40728°
Mean anomaly
64.7294°
Eccentric anomaly
78.32506°
Mean motion
2.72724 °/min
Orbital period
132 mins
BSTAR
0.00026196
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Other satellites on launch #90 in the year 2019 (2019-12-16 UTC)

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