CZ-6A DEB, 60676

Orbit data source: Space-Track

CZ-6A DEB, 60676 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/60676?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60676, 2024-140CD

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, 0.5 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 CZ-6A DEB
1 60676U 24140CD  26114.45293424  .00000211  00000-0  10119-3 0  9992
2 60676  88.9378 277.2770 0070681  22.9768 337.4553 14.13951917 88072

Epoch: 2026-04-24T10:52Z

TLE epoch observation values (Epoch: 2026-04-24T10:52:13.518Z)

Latitude

-0.00005°

Longitude

-98.26477°

Altitude

801.81 km

Speed

7.477 km/s

True Right ascension

18h 29m 06s

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

05:48:15

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

893.878 km

Perigee altitude

791.801 km

Semi-major axis

7,220.977 km

Eccentricity

0.00707

Inclination

88.9378°

RAAN

277.277°

Arg. of periapsis

22.9768°

True anomaly

337.14221°

Mean anomaly

337.4553°

Eccentric anomaly

337.29901°

Mean motion

3.53712 °/min

Orbital period

101.78 mins

BSTAR

0.00010119

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

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 60851 (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.
10 mins	2026-04-24 23:19:51.148Z	355.969° N	2026-04-24 23:24:51.148Z	275.267° WNW	43.676°	2026-04-24 23:29:51.148Z	190.968° SSW
8 mins	2026-04-25 10:46:51.148Z	148.527° SSE	2026-04-25 10:49:51.148Z	93.786° ESE	36.437°	2026-04-25 10:54:51.148Z	11.976° NNE
6 mins	2026-04-25 12:29:51.148Z	248.606° W	2026-04-25 12:31:51.148Z	274.874° WNW	17.572°	2026-04-25 12:35:51.148Z	324.229° NNW

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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, 60676 on other resources

View CZ-6A DEB, 60676 on Heavens-Above

View CZ-6A DEB, 60676 on Keep Track

View CZ-6A DEB, 60676 on Celestrak

View CZ-6A DEB, 60676 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, 60676

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-04-24T10:52:13.518Z)

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, 60676 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago