CZ-6A DEB, 60672

Orbit data source: Space-Track

CZ-6A DEB, 60672 is space debris in LEO originally from a launch on Tue, 06 Aug 2024 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/60672?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60672, 2024-140BZ

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (1 year ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.4 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 CZ-6A DEB
1 60672U 24140BZ  25344.75538735  .00010631  00000-0  12178-2 0  9995
2 60672  88.7367 274.4627 0152554 112.7134 249.0295 14.77717400 71923

Epoch: 2025-12-10T18:07Z

TLE epoch observation values (Epoch: 2025-12-10T18:07:45.467Z)

Latitude

-0.00007°

Longitude

-77.19791°

Altitude

679.393 km

Speed

7.496 km/s

True Right ascension

18h 17m 51s

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

02:56:55

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

740.372 km

Perigee altitude

526.444 km

Semi-major axis

7,011.545 km

Eccentricity

0.01526

Inclination

88.7367°

RAAN

274.4627°

Arg. of periapsis

112.7134°

True anomaly

247.40843°

Mean anomaly

249.0295°

Eccentric anomaly

248.21784°

Mean motion

3.69677 °/min

Orbital period

97.38 mins

BSTAR

0.0012178

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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB, 61298 (Decayed)

CZ-6A DEB, 60789 (Decayed)

CZ-6A DEB, 61140 (Decayed)

QIANFAN-15, 60393

QIANFAN-5, 60383

QIANFAN-4, 60382

CZ-6A DEB, 60665 (Decayed)

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CZ-6A DEB 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.
7 mins	2025-12-11 07:41:47.717Z	5.937° NNE	2025-12-11 07:44:47.717Z	51.273° ENE	42.733°	2025-12-11 07:48:47.717Z	174.814° S
6 mins	2025-12-11 20:15:47.717Z	200.613° SSW	2025-12-11 20:18:47.717Z	274.969° WNW	37.904°	2025-12-11 20:21:47.717Z	344.051° N

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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-6A DEB, 60672 on other resources

View CZ-6A DEB, 60672 on Heavens-Above

View CZ-6A DEB, 60672 on Keep Track

View CZ-6A DEB, 60672 on Celestrak

View CZ-6A DEB, 60672 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-6A DEB, 60672

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2025-12-10T18:07:45.467Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A DEB, 60672 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago