CZ-6A DEB, 61327

Orbit data source: Space-Track

CZ-6A DEB, 61327 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/61327?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61327, 2024-140UQ

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 (2 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 61327U 24140UQ  26171.22497660  .00058789  00000-0  12124-2 0  9992
2 61327  89.0636 266.3477 0068506  26.6703 333.8051 15.43111132 98740

Epoch: 2026-06-20T05:23Z

TLE epoch observation values (Epoch: 2026-06-20T05:23:57.978Z)

Latitude

-0°

Longitude

-83.08653°

Altitude

398.322 km

Speed

7.695 km/s

True Right ascension

17h 45m 23s

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

07:12:03

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

480.376 km

Perigee altitude

387.045 km

Semi-major axis

6,811.847 km

Eccentricity

0.00685

Inclination

89.0636°

RAAN

266.3477°

Arg. of periapsis

26.6703°

True anomaly

333.45589°

Mean anomaly

333.8051°

Eccentric anomaly

333.63076°

Mean motion

3.86052 °/min

Orbital period

93.25 mins

BSTAR

0.0012124

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

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 61310 (Decayed)

QIANFAN-4, 60382

QIANFAN-5, 60383

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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.
4 mins	2026-06-21 06:26:19.023Z	145.791° SSE	2026-06-21 06:28:19.023Z	83.509° E	30.788°	2026-06-21 06:30:19.023Z	23.307° NE
4 mins	2026-06-21 19:19:19.023Z	317.492° NNW	2026-06-21 19:21:19.023Z	266.536° W	21.969°	2026-06-21 19:23:19.023Z	227.074° WSW

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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, 61327 on other resources

View CZ-6A DEB, 61327 on Heavens-Above

View CZ-6A DEB, 61327 on Keep Track

View CZ-6A DEB, 61327 on Celestrak

View CZ-6A DEB, 61327 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, 61327

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-06-20T05:23:57.978Z)

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, 61327 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago