CZ-3B R/B, 44796

Orbit data source: Space-Track

CZ-3B R/B, 44796 is space debris in HEO originally from a launch on Sat, 23 Nov 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
44796, 2019-078D
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)
2019-11-23 (7 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: 1 day ago

TLE from 1 day ago
0 CZ-3B R/B
1 44796U 19078D   26265.16001726  .00000262  00000-0  27645-3 0  9996
2 44796  54.9647 331.4746 5404831 297.6240  18.2279  4.81677539118122
Epoch: 2026-09-22T03:50Z
TLE epoch observation values (Epoch: 2026-09-22T03:50:25.491Z)
Latitude
0.00007°
Longitude
-87.15306°
Altitude
2,016.791 km
Speed
8.25 km/s
True Right ascension
22h 05m 55s
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
01:44:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
16,436.871 km
Perigee altitude
427.443 km
Semi-major axis
14,810.294 km
Eccentricity
0.54048
Inclination
54.9647°
RAAN
331.4746°
Arg. of periapsis
297.624°
True anomaly
62.63205°
Mean anomaly
18.2279°
Eccentric anomaly
36.76139°
Mean motion
1.2042 °/min
Orbital period
298.95 mins
BSTAR
0.00027645
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Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)

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