CZ-4C R/B, 44623

Orbit data source: Space-Track

CZ-4C R/B, 44623 is space debris in SSO originally from a launch on Fri, 04 Oct 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
44623, 2019-066B
Orbit
SSO
Last TLE update
17 hours ago
Origin
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2019-10-04 (6 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
7.676 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 17 hours ago
0 CZ-4C R/B
1 44623U 19066B   25199.78698310  .00044855  00000-0  40588-3 0  9993
2 44623  97.7913 278.3575 0042721 226.7993 132.9695 15.66741688322181
Epoch: 2025-07-18T18:53Z
TLE epoch observation values (Epoch: 2025-07-18T18:53:15.339Z)
Latitude
-0.00005°
Longitude
58.21016°
Altitude
391.091 km
Speed
7.664 km/s
True Right ascension
18h 33m 25s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
61.1382°
Longitude
-106.69591°
Altitude
386.422 km
Speed
7.68 km/s
Apparent Right ascension
10h 59m 09s
Apparent Declination
16° 23' 16"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
01:04:57
Azimuth
34.019° NE
Elevation
-26.532°
Doppler factor
1
Orbital elements
Apogee altitude
393.963 km
Perigee altitude
336.347 km
Semi-major axis
6,743.292 km
Eccentricity
0.00427
Inclination
97.7913°
RAAN
278.3575°
Arg. of periapsis
226.7993°
True anomaly
133.32641°
Mean anomaly
132.9695°
Eccentric anomaly
133.14808°
Mean motion
3.91954 °/min
Orbital period
91.85 mins
BSTAR
0.00040588
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