CZ-3B R/B, 44205

Orbit data source: Space-Track

CZ-3B R/B, 44205 is space debris in HEO originally from a launch on Sat, 20 Apr 2019 UTC launched from the Xichang Space Center, China (XSC). 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
44205, 2019-023B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2019-04-20 (7 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 CZ-3B R/B
1 44205U 19023B   26171.00240989  .00243331  14630-7  11999-2 0  9997
2 44205  28.1876  99.1274 4772580 182.6063 173.6073  6.19995252 94064
Epoch: 2026-06-20T00:03Z
TLE epoch observation values (Epoch: 2026-06-20T00:03:28.214Z)
Latitude
0.00002°
Longitude
-169.96818°
Altitude
12,095.473 km
Speed
3.364 km/s
True Right ascension
06h 36m 29s
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
21:25:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
12,116.789 km
Perigee altitude
166.471 km
Semi-major axis
12,519.767 km
Eccentricity
0.47726
Inclination
28.1876°
RAAN
99.1274°
Arg. of periapsis
182.6063°
True anomaly
177.42421°
Mean anomaly
173.6073°
Eccentric anomaly
175.67126°
Mean motion
1.54935 °/min
Orbital period
232.36 mins
BSTAR
0.0011999
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Other satellites on launch #23 in the year 2019 (2019-04-20 UTC)

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