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 (1 year 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: 22 hours ago

TLE from 22 hours ago
0 CZ-3B R/B
1 63663U 25084B   26257.51434506  .00012938  00000-0  88492-3 0  9990
2 63663  27.0734 234.7573 6962857 179.2284 183.2140  2.72240662 12931
Epoch: 2026-09-14T12:20Z
TLE epoch observation values (Epoch: 2026-09-14T12:20:39.413Z)
Latitude
0.00001°
Longitude
56.08193°
Altitude
30,350.481 km
Speed
1.819 km/s
True Right ascension
15h 38m 57s
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
02:58:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,379.005 km
Perigee altitude
203.107 km
Semi-major axis
21,669.193 km
Eccentricity
0.69629
Inclination
27.0734°
RAAN
234.7573°
Arg. of periapsis
179.2284°
True anomaly
180.80185°
Mean anomaly
183.214°
Eccentric anomaly
181.89487°
Mean motion
0.68042 °/min
Orbital period
529.08 mins
BSTAR
0.00088492
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Other satellites on launch #84 in the year 2025 (2025-04-27 UTC)

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