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 (7 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: 5 days ago

TLE from 5 days ago
0 CZ-3C R/B
1 65487U 25196B   26083.76332973  .00007895  00000-0  12429-2 0  9991
2 65487  28.4119 291.2949 6945341 275.3762  15.3854  2.72476728  5463
Epoch: 2026-03-24T18:19Z
TLE epoch observation values (Epoch: 2026-03-24T18:19:11.688Z)
Latitude
-0.00009°
Longitude
-165.73507°
Altitude
4,148.592 km
Speed
7.571 km/s
True Right ascension
19h 25m 11s
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
17:54:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,319.533 km
Perigee altitude
237.184 km
Semi-major axis
21,656.495 km
Eccentricity
0.69453
Inclination
28.4119°
RAAN
291.2949°
Arg. of periapsis
275.3762°
True anomaly
84.2731°
Mean anomaly
15.3854°
Eccentric anomaly
42.02624°
Mean motion
0.68102 °/min
Orbital period
528.62 mins
BSTAR
0.0012429
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Other satellites on launch #196 in the year 2025 (2025-09-05 UTC)

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