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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44623 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
7.676 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 CZ-4C R/B
1 44623U 19066B 25250.21065864 .00089299 00000-0 61104-3 0 9999
2 44623 97.7861 334.4524 0035126 41.3135 319.0775 15.73626861330090Epoch: 2025-09-07T05:03Z
TLE epoch observation values (Epoch: 2025-09-07T05:03:20.906Z)
Latitude
-0.00005°
Longitude
-87.9181°
Altitude
333.871 km
Speed
7.718 km/s
True Right ascension
22h 17m 48s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:30:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
369.07 km
Perigee altitude
321.836 km
Semi-major axis
6,723.59 km
Eccentricity
0.00351
Inclination
97.7861°
RAAN
334.4524°
Arg. of periapsis
41.3135°
True anomaly
318.81296°
Mean anomaly
319.0775°
Eccentric anomaly
318.94532°
Mean motion
3.93678 °/min
Orbital period
91.45 mins
BSTAR
0.00061104
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Other satellites on launch #66 in the year 2019 (2019-10-04 UTC)
CZ-4C R/B Visibility
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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