CZ-6A DEB, 60682

Orbit data source: Space-Track

CZ-6A DEB, 60682 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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https://www.satcat.com/sats-embedded/60682?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60682, 2024-140CK

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 60682U 24140CK  26113.48056067  .00000409  00000-0  16899-3 0  9991
2 60682  89.0013 280.7866 0028841  19.0632 341.1633 14.24666535 88577

Epoch: 2026-04-23T11:32Z

TLE epoch observation values (Epoch: 2026-04-23T11:32:00.441Z)

Latitude

-0.00005°

Longitude

-103.74227°

Altitude

793.056 km

Speed

7.467 km/s

True Right ascension

18h 43m 08s

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

10:00:01

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

827.28 km

Perigee altitude

785.837 km

Semi-major axis

7,184.696 km

Eccentricity

0.00288

Inclination

89.0013°

RAAN

280.7866°

Arg. of periapsis

19.0632°

True anomaly

341.05623°

Mean anomaly

341.1633°

Eccentric anomaly

341.1098°

Mean motion

3.56394 °/min

Orbital period

101.01 mins

BSTAR

0.00016899

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

CZ-6A DEB, 61374 (Decayed)

CZ-6A DEB, 61328 (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.
9 mins	2026-04-24 11:14:52.435Z	162.868° S	2026-04-24 11:18:52.435Z	101.699° ESE	41.137°	2026-04-24 11:23:52.435Z	7.075° NNE
9 mins	2026-04-24 23:30:52.435Z	356.919° N	2026-04-24 23:34:52.435Z	307.957° NW	43.97°	2026-04-24 23:39:52.435Z	188.528° SSW

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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, 60682 on other resources

View CZ-6A DEB, 60682 on Heavens-Above

View CZ-6A DEB, 60682 on Keep Track

View CZ-6A DEB, 60682 on Celestrak

View CZ-6A DEB, 60682 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, 60682

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: 2026-04-23T11:32:00.441Z)

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, 60682 on other resources

Documentation

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