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 (9 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.4 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CZ-3B R/B
1 42663U 17018B   26257.80148537  .00010910  00000-0  98160-3 0  9994
2 42663  20.6479  14.0757 6722897 234.9612  42.8753  3.03954984 81578
Epoch: 2026-09-14T19:14Z
TLE epoch observation values (Epoch: 2026-09-14T19:14:08.335Z)
Latitude
-0.00001°
Longitude
91.74708°
Altitude
11,620.891 km
Speed
4.949 km/s
True Right ascension
00h 56m 14s
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
00:25:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
27,293.851 km
Perigee altitude
220.395 km
Semi-major axis
20,135.26 km
Eccentricity
0.67229
Inclination
20.6479°
RAAN
14.0757°
Arg. of periapsis
234.9612°
True anomaly
125.12994°
Mean anomaly
42.8753°
Eccentric anomaly
80.91102°
Mean motion
0.75964 °/min
Orbital period
473.91 mins
BSTAR
0.0009816
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Other satellites on launch #18 in the year 2017 (2017-04-12 UTC)

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