CZ-3B R/B, 42663

Orbit data source: Space-Track

CZ-3B R/B, 42663 is space debris in HEO originally from a launch on Wed, 12 Apr 2017 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
42663, 2017-018B
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)
2017-04-12 (8 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: 1 day ago

TLE from 1 day ago
0 CZ-3B R/B
1 42663U 17018B   25254.72066154  .00025658 -35664-7  12562-2 0  9993
2 42663  20.1995 216.5420 6834983 229.9694  46.8965  2.90099261 70587
Epoch: 2025-09-11T17:17Z
TLE epoch observation values (Epoch: 2025-09-11T17:17:45.157Z)
Latitude
0.00001°
Longitude
-33.92973°
Altitude
13,372.325 km
Speed
4.601 km/s
True Right ascension
14h 25m 56s
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
20:48:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
28,590.391 km
Perigee altitude
196.03 km
Semi-major axis
20,771.347 km
Eccentricity
0.6835
Inclination
20.1995°
RAAN
216.542°
Arg. of periapsis
229.9694°
True anomaly
130.09582°
Mean anomaly
46.8965°
Eccentric anomaly
85.96079°
Mean motion
0.72501 °/min
Orbital period
496.54 mins
BSTAR
0.0012562
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Other satellites on launch #18 in the year 2017 (2017-04-12 UTC)

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