CZ-6 R/B, 44784

Orbit data source: Space-Track

CZ-6 R/B, 44784 is space debris in LEO originally from a launch on Wed, 13 Nov 2019 UTC launched from the Taiyaun Space Center, China (TSC). 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
44784, 2019-076F
Orbit
LEO
Last TLE update
12 hours ago
Origin
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-6 STAGE 3, YF-85 X 4
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2019-11-13 (6 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.0 m
Radar Cross Section
9.057 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 12 hours ago
0 CZ-6 R/B
1 44784U 19076F   25199.47551142 -.00000366  00000-0 -10720-3 0  9995
2 44784  45.0087 343.0554 0087869 353.6899   6.2829 14.17976794294320
Epoch: 2025-07-18T11:24Z
TLE epoch observation values (Epoch: 2025-07-18T11:24:44.186Z)
Latitude
-0.00006°
Longitude
-124.65521°
Altitude
769.24 km
Speed
7.504 km/s
True Right ascension
22h 52m 13s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
44.77242°
Longitude
-46.40483°
Altitude
832.319 km
Speed
7.444 km/s
Apparent Right ascension
02h 18m 12s
Apparent Declination
6° 18' 54"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:25:46
Azimuth
324.104° NNW
Elevation
-37.003°
Doppler factor
1
Orbital elements
Apogee altitude
897.104 km
Perigee altitude
770.364 km
Semi-major axis
7,211.871 km
Eccentricity
0.00879
Inclination
45.0087°
RAAN
343.0554°
Arg. of periapsis
353.6899°
True anomaly
6.39431°
Mean anomaly
6.2829°
Eccentric anomaly
6.33848°
Mean motion
3.54382 °/min
Orbital period
101.59 mins
BSTAR
-0.0001072
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