CZ-3B R/B, 63663

Orbit data source: Space-Track

CZ-3B R/B, 63663 is space debris in HEO originally from a launch on Sun, 27 Apr 2025 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
63663, 2025-084B
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)
2025-04-27 (7 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 4.2 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 63663U 25084B   25341.40733851  .00014966  00000-0  11248-2 0  9993
2 63663  27.4437   0.6177 7124907 330.3675   3.5495  2.50834221  5515
Epoch: 2025-12-07T09:46Z
TLE epoch observation values (Epoch: 2025-12-07T09:46:34.047Z)
Latitude
0.00063°
Longitude
137.5642°
Altitude
604.874 km
Speed
9.835 km/s
True Right ascension
00h 02m 30s
True Declination
0° 00' 02"
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
08:40:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
32,812.098 km
Perigee altitude
201.494 km
Semi-major axis
22,884.933 km
Eccentricity
0.71249
Inclination
27.4437°
RAAN
0.6177°
Arg. of periapsis
330.3675°
True anomaly
29.05626°
Mean anomaly
3.5495°
Eccentric anomaly
12.12208°
Mean motion
0.62693 °/min
Orbital period
574.23 mins
BSTAR
0.0011248
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Other satellites on launch #84 in the year 2025 (2025-04-27 UTC)

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