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 (6 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: 2 days ago

TLE from 2 days ago
0 CZ-3B R/B
1 63663U 25084B   25288.24459628  .00014295  00000-0  11073-2 0  9993
2 63663  27.4269  22.6621 7134909 293.8910   9.6357  2.49473851  4186
Epoch: 2025-10-15T05:52Z
TLE epoch observation values (Epoch: 2025-10-15T05:52:13.118Z)
Latitude
0.00009°
Longitude
-89.44353°
Altitude
2,382.48 km
Speed
8.581 km/s
True Right ascension
01h 30m 31s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
23:58:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
32,977.394 km
Perigee altitude
202.416 km
Semi-major axis
22,968.042 km
Eccentricity
0.71349
Inclination
27.4269°
RAAN
22.6621°
Arg. of periapsis
293.891°
True anomaly
66.83387°
Mean anomaly
9.6357°
Eccentric anomaly
30.19782°
Mean motion
0.62353 °/min
Orbital period
577.36 mins
BSTAR
0.0011073
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Other satellites on launch #84 in the year 2025 (2025-04-27 UTC)

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