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 (10 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 8.0 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CZ-3C R/B
1 65487U 25196B   26177.82877262  .00007602  00000-0  13885-2 0  9990
2 65487  28.2785 248.2699 6932251 345.6298   2.0337  2.73836457  8030
Epoch: 2026-06-26T19:53Z
TLE epoch observation values (Epoch: 2026-06-26T19:53:25.954Z)
Latitude
-0.00037°
Longitude
34.97238°
Altitude
320.017 km
Speed
10.027 km/s
True Right ascension
16h 33m 07s
True Declination
0° 00' 01"
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
07:29:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,169.732 km
Perigee altitude
243.528 km
Semi-major axis
21,584.767 km
Eccentricity
0.69323
Inclination
28.2785°
RAAN
248.2699°
Arg. of periapsis
345.6298°
True anomaly
15.42058°
Mean anomaly
2.0337°
Eccentric anomaly
6.59638°
Mean motion
0.68442 °/min
Orbital period
525.99 mins
BSTAR
0.0013885
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Other satellites on launch #196 in the year 2025 (2025-09-05 UTC)

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