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 (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 44796U 19078D   25360.28807815  .00000942  00000-0  11446-2 0  9993
2 44796  54.9222 132.9307 5387848 206.0129 112.2778  4.81490963105125
Epoch: 2025-12-26T06:54Z
TLE epoch observation values (Epoch: 2025-12-26T06:54:49.952Z)
Latitude
-0°
Longitude
-65.81208°
Altitude
14,018.848 km
Speed
3.49 km/s
True Right ascension
08h 51m 42s
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
11:38:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
16,417.614 km
Perigee altitude
454.363 km
Semi-major axis
14,814.125 km
Eccentricity
0.53878
Inclination
54.9222°
RAAN
132.9307°
Arg. of periapsis
206.0129°
True anomaly
154.05012°
Mean anomaly
112.2778°
Eccentric anomaly
134.3518°
Mean motion
1.20373 °/min
Orbital period
299.07 mins
BSTAR
0.0011446
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Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)

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