CZ-3B R/B, 63076

Orbit data source: Space-Track

CZ-3B R/B, 63076 is space debris in HEO originally from a launch on Sat, 22 Feb 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
63076, 2025-036B
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)
2025-02-22 (1 year 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: 3 days ago

TLE from 3 days ago
0 CZ-3B R/B
1 63076U 25036B   26167.56978722  .00205035  43242-6  32039-2 0  9991
2 63076  27.0310 138.9850 6981661 138.1571 304.3408  2.72346138 11532
Epoch: 2026-06-16T13:40Z
TLE epoch observation values (Epoch: 2026-06-16T13:40:29.615Z)
Latitude
-0.00003°
Longitude
28.99909°
Altitude
16,720.894 km
Speed
4.014 km/s
True Right ascension
09h 15m 50s
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
22:24:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,410.312 km
Perigee altitude
160.682 km
Semi-major axis
21,663.634 km
Eccentricity
0.69817
Inclination
27.031°
RAAN
138.985°
Arg. of periapsis
138.1571°
True anomaly
221.92301°
Mean anomaly
304.3408°
Eccentric anomaly
264.52155°
Mean motion
0.68069 °/min
Orbital period
528.88 mins
BSTAR
0.0032039
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Other satellites on launch #36 in the year 2025 (2025-02-22 UTC)

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