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: 8 hours ago

TLE from 8 hours ago
0 CZ-3B R/B
1 44796U 19078D   25307.97214455  .00000449  00000-0  50715-3 0  9997
2 44796  54.9117 164.0608 5385232 188.2260 157.1923  4.81420077102609
Epoch: 2025-11-03T23:19Z
TLE epoch observation values (Epoch: 2025-11-03T23:19:53.289Z)
Latitude
-0.00001°
Longitude
130.62463°
Altitude
16,145.945 km
Speed
2.914 km/s
True Right ascension
10h 56m 15s
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
03:32:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
16,415.978 km
Perigee altitude
458.91 km
Semi-major axis
14,815.581 km
Eccentricity
0.53852
Inclination
54.9117°
RAAN
164.0608°
Arg. of periapsis
188.226°
True anomaly
171.81686°
Mean anomaly
157.1923°
Eccentric anomaly
165.11721°
Mean motion
1.20355 °/min
Orbital period
299.11 mins
BSTAR
0.00050715
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Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)

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