DECAYED

CZ-4B R/B, 67132 (Decayed)

Orbit data source: Space-Track

CZ-4B R/B, 67132 was space debris in LEO 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.

Not visible in the next 10 days

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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

Decayed

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Decayed spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

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

Launch date (UTC)

2025-12-16 (4 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 8.0 m

Radar Cross Section

14.536 m²

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

TLE from 3 weeks ago

0 CZ-4B R/B
1 67132U 25300B   26076.27513352  .10806986  25818-5  16944-3 0  9992
2 67132  97.5078 164.4332 0011095  21.5932 338.5837 16.47808531 14429

Epoch: 2026-03-17T06:36Z

TLE epoch observation values (Epoch: 2026-03-17T06:36:11.536Z)

Latitude

0.00002°

Longitude

-109.47047°

Altitude

141.633 km

Speed

7.825 km/s

True Right ascension

10h 57m 43s

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

18:02:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

149.149 km

Perigee altitude

134.681 km

Semi-major axis

6,520.052 km

Eccentricity

0.00111

Inclination

97.5078°

RAAN

164.4332°

Arg. of periapsis

21.5932°

True anomaly

338.53722°

Mean anomaly

338.5837°

Eccentric anomaly

338.56046°

Mean motion

4.12256 °/min

Orbital period

87.32 mins

BSTAR

0.00016944

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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

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This satellite is decayed.

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 (Decayed) on other resources

View CZ-4B R/B, 67132 (Decayed) on Celestrak

View CZ-4B R/B, 67132 (Decayed) 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 (Decayed)

Orbit data source: Space-Track

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

TLE from 3 weeks ago

TLE epoch observation values (Epoch: 2026-03-17T06:36:11.536Z)

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

Co-orbital & Co-planar RSOs

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

Documentation

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