CZ-4B R/B, 67132

Orbit data source: Space-Track

CZ-4B R/B, 67132 is space debris in SSO originally from a launch on Tue, 16 Dec 2025 UTC launched from the Taiyaun Space Center, China (TSC). 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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Iframe URL

https://www.satcat.com/sats-embedded/67132?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

67132, 2025-300B

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

~1,000 kg wet, ~1,000 kg dry

Launch date (UTC)

2025-12-16 (6 days ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

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Last TLE update: 3 days ago

TLE from 3 days ago

0 CZ-4B R/B
1 67132U 25300B   25352.67574779  .00040543  26530-5  19566-3 0  9995
2 67132  97.5563  66.9660 0174197   9.3582 351.0851 15.63831828   407

Epoch: 2025-12-18T16:13Z

TLE epoch observation values (Epoch: 2025-12-18T16:13:04.609Z)

Latitude

0.00005°

Longitude

96.16895°

Altitude

263.526 km

Speed

7.815 km/s

True Right ascension

04h 27m 51s

True Declination

0° 00' 00"

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

12:16:48

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

491.125 km

Perigee altitude

255.902 km

Semi-major axis

6,751.65 km

Eccentricity

0.01742

Inclination

97.5563°

RAAN

66.966°

Arg. of periapsis

9.3582°

True anomaly

350.76897°

Mean anomaly

351.0851°

Eccentric anomaly

350.92772°

Mean motion

3.91226 °/min

Orbital period

92.02 mins

BSTAR

0.00019566

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Other satellites on launch #300 in the year 2025 (2025-12-16 UTC)

ZY 3 04, 67131

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CZ-4B R/B Visibility forecast

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Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
5 mins	2025-12-21 18:28:50.000Z	340.254° N	2025-12-21 18:30:50.000Z	273.491° WNW	30.823°	2025-12-21 18:33:50.000Z	217.902° SW

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out CZ-4B R/B, 67132 on other resources

View CZ-4B R/B, 67132 on Heavens-Above

View CZ-4B R/B, 67132 on Keep Track

View CZ-4B R/B, 67132 on Celestrak

View CZ-4B R/B, 67132 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-4B R/B, 67132

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-12-18T16:13:04.609Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #300 in the year 2025 (2025-12-16 UTC)

CZ-4B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B R/B, 67132 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago