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, 6.2 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 42663U 17018B   26171.27751896  .00011026  00000-0  10229-2 0  9996
2 42663  20.4471  61.9051 6733637 148.5644 279.8739  3.02391109 78941
Epoch: 2026-06-20T06:39Z
TLE epoch observation values (Epoch: 2026-06-20T06:39:37.638Z)
Latitude
0.00003°
Longitude
53.48027°
Altitude
19,590.756 km
Speed
3.311 km/s
True Right ascension
04h 07m 31s
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
21:34:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
27,431.555 km
Perigee altitude
221.428 km
Semi-major axis
20,204.628 km
Eccentricity
0.67336
Inclination
20.4471°
RAAN
61.9051°
Arg. of periapsis
148.5644°
True anomaly
211.39879°
Mean anomaly
279.8739°
Eccentric anomaly
244.92819°
Mean motion
0.75573 °/min
Orbital period
476.36 mins
BSTAR
0.0010229
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Other satellites on launch #18 in the year 2017 (2017-04-12 UTC)

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