DECAYED

CZ-4B R/B, 44888 (Decayed)

Orbit data source: Space-Track

CZ-4B R/B, 44888 was space debris in LEO originally from a launch on Fri, 20 Dec 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.

Not visible in the next 10 days
Identifier
44888, 2019-093K
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2019-12-20 (6 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.5 m
Radar Cross Section
14.536 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 weeks ago

TLE from 3 weeks ago
0 CZ-4B R/B
1 44888U 19093K   26027.55977014  .12931397  31025-5  15746-3 0  9996
2 44888  97.8978 264.4595 0005230 211.4432 148.6559 16.49894650340225
Epoch: 2026-01-27T13:26Z
TLE epoch observation values (Epoch: 2026-01-27T13:26:04.140Z)
Latitude
-0.00002°
Longitude
-63.89717°
Altitude
145.774 km
Speed
7.817 km/s
True Right ascension
17h 37m 50s
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
16:35:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
139.838 km
Perigee altitude
133.024 km
Semi-major axis
6,514.568 km
Eccentricity
0.00052
Inclination
97.8978°
RAAN
264.4595°
Arg. of periapsis
211.4432°
True anomaly
148.68706°
Mean anomaly
148.6559°
Eccentric anomaly
148.67148°
Mean motion
4.12776 °/min
Orbital period
87.21 mins
BSTAR
0.00015746
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