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 (5 months 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: 6 days ago

TLE from 6 days ago
0 CZ-3B R/B
1 63663U 25084B   25252.89663685  .00017910 -77243-6  12258-2 0  9998
2 63663  27.4161  37.3104 7145026 269.6318  16.0735  2.48331557  3299
Epoch: 2025-09-09T21:31Z
TLE epoch observation values (Epoch: 2025-09-09T21:31:09.423Z)
Latitude
-0.00045°
Longitude
85.30341°
Altitude
4,941.071 km
Speed
7.288 km/s
True Right ascension
02h 29m 05s
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
15:45:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,121.288 km
Perigee altitude
199.271 km
Semi-major axis
23,038.416 km
Eccentricity
0.7145
Inclination
27.4161°
RAAN
37.3104°
Arg. of periapsis
269.6318°
True anomaly
90.91653°
Mean anomaly
16.0735°
Eccentric anomaly
45.04248°
Mean motion
0.62067 °/min
Orbital period
580.01 mins
BSTAR
0.0012258
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Other satellites on launch #84 in the year 2025 (2025-04-27 UTC)

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