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
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 CZ-4C R/B
1 44623U 19066B 25323.92551573 .00437126 88031-4 71796-3 0 9993
2 44623 97.7746 58.1302 0013764 123.8357 236.4234 16.03015796341763Epoch: 2025-11-19T22:12Z
TLE epoch observation values (Epoch: 2025-11-19T22:12:44.559Z)
Latitude
0.00001°
Longitude
25.75428°
Altitude
274.331 km
Speed
7.74 km/s
True Right ascension
03h 52m 31s
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
03:28:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
272.086 km
Perigee altitude
253.804 km
Semi-major axis
6,641.082 km
Eccentricity
0.00138
Inclination
97.7746°
RAAN
58.1302°
Arg. of periapsis
123.8357°
True anomaly
236.29212°
Mean anomaly
236.4234°
Eccentric anomaly
236.35775°
Mean motion
4.01037 °/min
Orbital period
89.77 mins
BSTAR
0.00071796
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Other satellites on launch #66 in the year 2019 (2019-10-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-4C R/B Visibility
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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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| CZ-4C R/B is likely not visible in the next few days. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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