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: 2 days ago

TLE from 2 days ago
0 CZ-3B R/B
1 44796U 19078D   25259.18279709  .00000109  00000-0  28974-3 0  9994
2 44796  54.8993 193.0881 5384797 171.7373 203.1814  4.81382330100251
Epoch: 2025-09-16T04:23Z
TLE epoch observation values (Epoch: 2025-09-16T04:23:13.668Z)
Latitude
-0.00004°
Longitude
131.89982°
Altitude
16,141.303 km
Speed
2.916 km/s
True Right ascension
12h 52m 20s
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
19:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
16,416.527 km
Perigee altitude
459.912 km
Semi-major axis
14,816.357 km
Eccentricity
0.53848
Inclination
54.8993°
RAAN
193.0881°
Arg. of periapsis
171.7373°
True anomaly
188.32014°
Mean anomaly
203.1814°
Eccentric anomaly
195.12905°
Mean motion
1.20346 °/min
Orbital period
299.14 mins
BSTAR
0.00028974
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Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)

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