CZ-3C R/B, 65487

Orbit data source: Space-Track

CZ-3C R/B, 65487 is space debris in HEO originally from a launch on Fri, 05 Sep 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
65487, 2025-196B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3C STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2025-09-05 (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: 21 hours ago

TLE from 21 hours ago
0 CZ-3C R/B
1 65487U 25196B   26313.33123188  .00042967 -10136-6  17941-2 0  9997
2 65487  27.9799 184.7844 6927833  88.9032 342.8923  2.77897340 11762
Epoch: 2026-11-09T07:56Z
TLE epoch observation values (Epoch: 2026-11-09T07:56:58.434Z)
Latitude
-0.00001°
Longitude
17.1335°
Altitude
4,565.812 km
Speed
7.361 km/s
True Right ascension
12h 19m 32s
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
01:10:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
29,803.539 km
Perigee altitude
188.336 km
Semi-major axis
21,374.075 km
Eccentricity
0.69278
Inclination
27.9799°
RAAN
184.7844°
Arg. of periapsis
88.9032°
True anomaly
271.12601°
Mean anomaly
342.8923°
Eccentric anomaly
314.65738°
Mean motion
0.69456 °/min
Orbital period
518.31 mins
BSTAR
0.0017941
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Other satellites on launch #196 in the year 2025 (2025-09-05 UTC)

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